Index

_

__init__() (Additive_Solver method), [1], [2] (Constants method) (Container method) (ContainerOrdered method) (Coolant_Line method) (Cubic_Spline_Blender method) (Data method) (DataOrdered method) (Diffed_Data method) (Distance method), [1], [2] (Evaluate method) (expanded_array method) (FixPointNormalize method), [1] (folder method), [1], [2] (Geodesic method), [1], [2] (Geodesic_Calculate method), [1], [2] (GeodesicCapability method) (Liquid_Cooled_Wavy_Channel method) (Math method) (output method), [1], [2] (Process_Geometry method) (Property method) (Trust_Region method) (Trust_Region_Optimization method) (Vehicle method), [1]

_base (Config attribute) _diff (Config attribute)

A

a (Geodesic attribute), [1] A_F_st_Jet_A (Reformer attribute) A_max_function() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) A_min_function() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) A_PZ (Combustor attribute) A_SZ (Combustor attribute) A_weighting_metric() (in module RCAIDE.Library.Methods.Noise.Metrics.A_weighting_metric) absolute_sensible_enthalpy (Combustor attribute) acceleration() (in module RCAIDE.Library.Mission.Common.Update.acceleration) accessories (System attribute) accuracy_ratio() (Trust_Region_Optimization method), [1] Acrylic (class in RCAIDE.Library.Attributes.Materials.Acrylic) active (Coolant_Line attribute) (Electrical_Bus attribute) (Fuel_Line attribute) (Propulsor attribute) active_crypgenic_tanks_tanks (Electric_Rotor attribute) (Turbofan attribute) (Turboshaft attribute) Actuator_Disk_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Actuator_Disc_Theory.Actuator_Disk_performance) add_mission_variables() (in module RCAIDE.Library.Mission.Solver.converge) add_segment_sources() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.write_vsp_mesh) add_span_break() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) add_unknowns_and_residuals_to_segment() (Network method) Additive_Solve() (Additive_Solver method), [1] Additive_Solver (class in RCAIDE.Framework.Optimization.Packages.additive.additive_setup), [1] aero_coeff() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.aero_coeff) aerodynamic_center (Boom attribute) (Fuselage attribute) (Nacelle attribute) (Wing attribute) Aerodynamics (class in RCAIDE.Framework.Analyses.Aerodynamics.Aerodynamics) aerodynamics() (in module RCAIDE.Library.Mission.Common.Pre_Process.aerodynamics) (in module RCAIDE.Library.Mission.Common.Update.aerodynamics) aft_centerbody_area (Blended_Wing_Body_Fuselage attribute) aft_centerbody_taper (Blended_Wing_Body_Fuselage attribute) afterburner (Turbojet attribute) afterburner_active (Turbojet attribute) Aileron (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Aileron) Air (class in RCAIDE.Library.Attributes.Gases.Air) air (Cross_Flow_Heat_Exchanger attribute) air_chemical_properties (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Methane attribute) Air_Cooled (class in RCAIDE.Library.Components.Thermal_Management.Batteries.Air_Cooled) air_cooled_performance() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.air_cooled_performance) air_hydraulic_diameter (Cross_Flow_Heat_Exchanger attribute) Aircraft (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Aircraft) aircraft_aerodynamic_analysis() (in module RCAIDE.Library.Methods.Performance.aircraft_aerodynamic_analysis) Airfoil (Body_of_Revolution_Nacelle attribute) (class in RCAIDE.Library.Components.Airfoils.Airfoil) (Segment attribute) (Wing attribute) airfoil_analysis() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.airfoil_analysis) Airfoil_Container (class in RCAIDE.Library.Components.Powertrain.Converters.Rotor) airfoil_polar_stations (Rotor attribute) Airfoils (Rotor attribute) airframe_noise() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.airframe_noise) Alcohol_Mixture (class in RCAIDE.Library.Attributes.Propellants.Alcohol_Mixture) Alkane_Mixture (class in RCAIDE.Library.Attributes.Propellants.Alkane_Mixture) ALL (Geodesic attribute), [1] (GeodesicCapability attribute), [1] all_constraints() (Nexus method) All_Moving_Surface (class in RCAIDE.Library.Components.Wings.All_Moving_Surface) alphac (Combustor attribute) altitude() (in module RCAIDE.Library.Mission.Common.Update.altitude) Aluminum (class in RCAIDE.Library.Attributes.Materials.Aluminum) Aluminum_Air (class in RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Aluminum_Air) Aluminum_Alloy (class in RCAIDE.Library.Attributes.Materials.Aluminum_Alloy) aluminum_mass_factor (Aluminum_Air.cell attribute) amplitude_function_delta_K_1() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) amplitude_function_K_1() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) amplitude_function_K_2() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) analyses_setup() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) Analysis (class in RCAIDE.Framework.Analyses.Analysis) Analysis.Container (class in RCAIDE.Framework.Analyses.Analysis) AngDiff() (Math static method), [1] angle_of_attack_effect() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.angle_of_attack_effect), [1] angles_to_dcms() (in module RCAIDE.Framework.Core.Utilities), [1] AngNormalize() (Math static method), [1] AngRound() (Math static method), [1] angular_acceleration() (in module RCAIDE.Library.Mission.Common.Update.angular_acceleration) angular_velocity (Fan attribute) antoine_coefficients (Liquid_Hydrogen attribute) append() (Container method), [1] (ContainerOrdered method) (Data method) (DataOrdered method) (Diffed_Data.Container method) (Segment_Container method) (Vehicle method) (Vehicle_Mass_Container method) append_air_cooled_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.append_air_cooled_conditions) append_air_cooled_segment_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.append_air_cooled_conditions) append_airfoil() (Body_of_Revolution_Nacelle method) (Rotor method) (Segment method) (Wing method) append_array() (in module RCAIDE.Framework.Mission.Common.State) append_avionics_conditions() (in module RCAIDE.Library.Methods.Powertrain.Systems.append_avionics_conditions) append_avl_wing_control_surfaces() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures), [1] append_battery_conditions() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.append_battery_conditions) append_battery_segment_conditions() (Generic_Battery_Module method) (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.append_battery_conditions) append_body() (Aircraft method) append_bus_conditions() (in module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.append_bus_conditions) append_bus_segment_conditions() (in module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.append_bus_conditions) append_cabin() (Fuselage method) append_cabin_class() (Cabin method) append_case() (Container method) (Ducted_Fan_Design_Code method) (Run_Case.Container method) append_combustor_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Combustor.append_combustor_conditions) append_component() (Vehicle method) append_compression_nozzle_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Compression_Nozzle.append_compression_nozzle_conditions) append_compressor_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Compressor.append_compressor_conditions) append_constant_speed_internal_combustion_engine_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.append_constant_speed_internal_combustion_engine_conditions) append_control_surface() (Section method) (Wing method) append_control_surface_result() (Control_Surface_Data method) append_cross_flow_heat_exchanger_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.append_cross_flow_heat_exchanger_conditions) append_cross_flow_hex_segment_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.append_cross_flow_heat_exchanger_conditions) append_cryogenic_tank_conditions() (in module RCAIDE.Library.Methods.Powertrain.Sources.Cryogenic_Tanks.append_cryogenic_tank_conditions) append_duct_airfoil() (Ducted_Fan method) append_ducted_fan_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.append_ducted_fan_conditions) append_electric_ducted_fan_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.append_electric_ducted_fan_conditions) append_electric_ducted_fan_residual_and_unknown() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.append_electric_ducted_fan_residual_and_unknown), [1] append_electric_rotor_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.append_electric_rotor_conditions)

append_electric_rotor_residual_and_unknown() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.append_electric_rotor_residual_and_unknown) append_energy_network() (Vehicle method) append_engine_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Engine.append_engine_conditions) append_esc_conditions() (in module RCAIDE.Library.Methods.Powertrain.Modulators.Electronic_Speed_Controller.append_esc_conditions) append_expansion_nozzle_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Expansion_Nozzle.append_expansion_nozzle_conditions) append_fan_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fan.append_fan_conditions) append_fuel_cell_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.append_fuel_cell_conditions) (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.append_fuel_cell_conditions) append_fuel_cell_segment_conditions() (Generic_Fuel_Cell_Stack method) (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.append_fuel_cell_conditions) (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.append_fuel_cell_conditions) (Proton_Exchange_Membrane_Fuel_Cell method) append_fuel_tank() (Fuselage method) (Wing method) append_fuel_tank_conditions() (in module RCAIDE.Library.Methods.Powertrain.Sources.Fuel_Tanks.append_fuel_tank_conditions) append_generator_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.append_generator_conditions) append_hub_airfoil() (Ducted_Fan method) append_internal_combustion_engine_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.append_internal_combustion_engine_conditions) append_internal_combustion_engine_residual_and_unknown() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.append_internal_combustion_engine_residual_and_unknown) append_mission() (Missions method) append_motor_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.append_motor_conditions) append_operating_conditions() (Air_Cooled method) (Airfoil method) (Avionics method) (Central_Fuel_Tank method) (Combustor method) (Compression_Nozzle method) (Compressor method) (Constant_Speed_Internal_Combustion_Engine method) (Cross_Flow_Heat_Exchanger method) (Cryogenic_Tank method) (DC_Generator method) (DC_Motor method) (Ducted_Fan method) (Electric_Ducted_Fan method) (Electric_Rotor method) (Electrical_Bus method) (Electronic_Speed_Controller method) (Engine method) (Expansion_Nozzle method) (Fan method) (Fuel_Tank method) (Generic_Battery_Module method) (Generic_Fuel_Cell_Stack method) (Internal_Combustion_Engine method) (Liquid_Cooled_Wavy_Channel method) (Nacelle method) (Payload method) (PMSM_Generator method) (PMSM_Motor method) (Proton_Exchange_Membrane_Fuel_Cell method) (Ram method) (Reservoir method) (Rotor method) (Supersonic_Nozzle method) (Turbine method) (Turboelectric_Generator method) (Turbofan method) (Turbojet method) (Turboprop method) (Turboshaft method) (Wing_Fuel_Tank method) append_payload_conditions() (in module RCAIDE.Library.Methods.Powertrain.Systems.append_payload_conditions) append_propulsor_unknowns_and_residuals() (Constant_Speed_Internal_Combustion_Engine method) (Electric_Ducted_Fan method) (Electric_Rotor method) (Internal_Combustion_Engine method) (Turbofan method) (Turbojet method) (Turboprop method) (Turboshaft method) append_ram_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ram.append_ram_conditions) append_reservoir_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.append_reservoir_conditions) append_reservoir_segment_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.append_reservoir_conditions) append_rotor_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.append_rotor_conditions) append_section() (Body method) (Wing method) append_segment() (Boom method) (Container method) (Fuselage method) (Segment.Container method) (Stack_Nacelle method) (Wing method) append_segment_conditions() (Air_Cooled method) (Cross_Flow_Heat_Exchanger method) (Electrical_Bus method) (Liquid_Cooled_Wavy_Channel method) (Reservoir method) append_supersonic_nozzle_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Supersonic_Nozzle.append_supersonic_nozzle_conditions) append_turbine_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turbine.append_turbine_conditions) append_turboelectric_generator_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.append_turboelectric_generator_conditions) append_turbofan_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.append_turbofan_conditions) append_turbojet_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.append_turbojet_conditions) append_turboprop_conditions() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.append_turboprop_conditions) append_turboshaft_conditions() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.append_turboshaft_conditions) append_wavy_channel_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.append_wavy_channel_conditions) append_wavy_channel_segment_conditions() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.append_wavy_channel_conditions) append_wing() (Aircraft method) apply_pre_stall_data() (in module RCAIDE.Library.Methods.Geometry.Airfoil.compute_airfoil_properties) apply_properties() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.get_fuel_tank_properties) AREA (Geodesic attribute), [1] (GeodesicCapability attribute), [1] area_ratio (Combustor attribute) areas (Boom attribute) (Fuselage attribute) (Nacelle attribute) (Segment attribute) (Turbojet attribute) (Wing attribute) aspect_ratio (Wing attribute) assigned_propulsors (Electrical_Bus attribute) (Fuel_Line attribute) asymmetry_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.asymmetry_drag) Athena_Vortex_Lattice (class in RCAIDE.Framework.Analyses.Aerodynamics.Athena_Vortex_Lattice) (class in RCAIDE.Framework.Analyses.Stability.Athena_Vortex_Lattice) atleast_2d() (in module RCAIDE.Framework.Core.Arrays), [1] atleast_2d_col() (in module RCAIDE.Framework.Core.Arrays), [1] atleast_2d_row() (in module RCAIDE.Framework.Core.Arrays), [1] Atmosphere (class in RCAIDE.Library.Attributes.Atmospheres.Atmosphere) atmosphere() (in module RCAIDE.Library.Mission.Common.Update.atmosphere) Atmospheric (class in RCAIDE.Framework.Analyses.Atmospheric.Atmospheric) atmospheric_attenuation() (in module RCAIDE.Library.Methods.Noise.Common.atmospheric_attenuation) Aviation_Gasoline (class in RCAIDE.Library.Attributes.Propellants.Aviation_Gasoline) Avionics (class in RCAIDE.Library.Components.Powertrain.Systems.Avionics) avionics (Electrical_Bus attribute) axial_fuel_velocity_ratio (Combustor attribute) axial_gap_to_radius_of_rotor (PMSM_Motor attribute) AZIMUTH (Geodesic attribute), [1] (GeodesicCapability attribute), [1]

B

B_max_function() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) B_min_function() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) background_noise() (in module RCAIDE.Library.Methods.Noise.Common.background_noise) base_analysis() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) base_mission_setup() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) Battery_Discharge (class in RCAIDE.Framework.Mission.Segments.Ground.Battery_Discharge) battery_module_electric_configuration (Electrical_Bus attribute) battery_modules (Coolant_Line attribute) (Electrical_Bus attribute) Battery_Recharge (class in RCAIDE.Framework.Mission.Segments.Ground.Battery_Recharge) BEMT_Helmholtz_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.BEMT_Helmholtz_performance) BEMT_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.BEMT_performance) Biconvex_Airfoil (class in RCAIDE.Library.Components.Airfoils.Biconvex_Airfoil) Bidirectional_Carbon_Fiber (class in RCAIDE.Library.Attributes.Materials.Bidirectional_Carbon_Fiber) blade_clearance (Ducted_Fan attribute) blade_geometry_setup() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.blade_geometry_setup) blade_pitch_command (Rotor attribute) blade_solidity (Rotor attribute) Blended_Wing_Body_Fuselage (class in RCAIDE.Library.Components.Fuselages.Blended_Wing_Body_Fuselage) BMS_additional_weight_factor (Generic_Battery_Module attribute) Body (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Body) Body_of_Revolution_Nacelle (class in RCAIDE.Library.Components.Nacelles.Body_of_Revolution_Nacelle)

body_to_nac_vel() (Nacelle method) body_to_prop_vel() (Ducted_Fan method) (Rotor method) Boom (class in RCAIDE.Library.Components.Booms.Boom) Boom.Container (class in RCAIDE.Library.Components.Booms.Boom) BPM_boundary_layer_properties() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.BPM_boundary_layer_properties) breaks (Constant_Temperature attribute) (US_Standard_1976 attribute) broadband_noise() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.broadband_noise) build_AVL_surrogates() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.build_AVL_surrogates) build_CRN_EI_surrogates() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.build_CRN_EI_surrogates) build_data_r() (in module RCAIDE.load) build_dict_base() (in module RCAIDE.save) build_dict_r() (in module RCAIDE.save) build_RHS() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_RHS_matrix) build_surrogate() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.build_VLM_surrogates) build_VLM_surrogates() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.build_VLM_surrogates) burner_drag_coefficient (Combustor attribute) Business (class in RCAIDE.Library.Components.Fuselages.Cabins.Classes.Business) Butanol (class in RCAIDE.Library.Attributes.Propellants.Butanol) bypass_ratio (Turbofan attribute) (Turbojet attribute)

C

c_electrical (Copper attribute) c_thermal (Copper attribute) Cabin (class in RCAIDE.Library.Components.Fuselages.Cabins.Cabin) cabin_area (Blended_Wing_Body_Fuselage attribute) calculate_activation_losses() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_concentration_losses_HT() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_concentration_losses_LT() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_constraint_violation() (Trust_Region_Optimization method), [1] calculate_correction() (Trust_Region_Optimization method), [1] Calculate_Distance() (in module RCAIDE.Framework.Analyses.Geodesics.Geodesics), [1] calculate_E_cell() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_emission_indices() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_cantera) calculate_limiting_current_density_HT() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_limiting_current_density_LT() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_load() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) calculate_ohmic_losses_HT() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_ohmic_losses_LT() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_P_drop_hum() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_P_drop_stack() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_P_H2() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_P_O2() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) calculate_voltage() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) call_avl() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.run_AVL_analysis) CAP_ALL (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_C1 (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_C1p (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_C2 (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_C3 (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_C4 (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_MASK (Geodesic attribute), [1] (GeodesicCapability attribute), [1] CAP_NONE (Geodesic attribute), [1] (GeodesicCapability attribute), [1] capacity (Generic_Battery_Module attribute) Carbon_Fiber_Honeycomb (class in RCAIDE.Library.Attributes.Materials.Carbon_Fiber_Honeycomb) cbrt() (Math static method), [1] cell (Generic_Battery_Module attribute) (Lithium_Ion_LFP attribute) (Lithium_Ion_NMC attribute) center_of_gravity (Mass_Properties attribute) Central_Fuel_Tank (class in RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks.Central_Fuel_Tank) cf_filter() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.cf_filter) characteristic_length_of_flow (PMSM_Motor attribute) charging_c_rate (Electrical_Bus attribute) chebyshev_data() (in module RCAIDE.Library.Methods.Utilities.Chebyshev.chebyshev_data) check_tags() (in module RCAIDE.Framework.Core.Container) chord_distribution (Rotor attribute) chord_fraction (Control_Surface attribute) chords (Segment attribute) (Wing attribute) chordwise_distribution() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.chordwise_distribution) Circle_Segment (class in RCAIDE.Library.Components.Fuselages.Segments.Circle_Segment) clean_data() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.design_ducted_fan) clean_wing_noise() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.clean_wing_noise) clear() (DataOrdered method) Climb (class in RCAIDE.Framework.Mission.Segments.Vertical_Flight.Climb) clockwise_rotation (Rotor attribute) CO2 (class in RCAIDE.Library.Attributes.Gases.CO2) colorax() (in module RCAIDE.Library.Plots.Noise.plot_2D_noise_contour) (in module RCAIDE.Library.Plots.Noise.plot_3D_noise_contour) combustion_temperature (Rocket_LH2 attribute) (Rocket_RP1 attribute) Combustor (class in RCAIDE.Library.Components.Powertrain.Converters.Combustor) combustor (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) Component (class in RCAIDE.Library.Components.Component) Component.Container (class in RCAIDE.Library.Components.Component) composition (Air attribute) (Atmosphere attribute) (CO2 attribute) (Gas attribute) (Steam attribute) compressibility_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressibility_drag) compressibility_effects (Compression_Nozzle attribute) compressibility_factor (Gaseous_Hydrogen attribute) compressible_mixed_flat_plate() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressible_mixed_flat_plate) compressible_turbulent_flat_plate() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressible_turbulent_flat_plate) compression_levels (Compression_Nozzle attribute) Compression_Nozzle (class in RCAIDE.Library.Components.Powertrain.Converters.Compression_Nozzle) Compressor (class in RCAIDE.Library.Components.Powertrain.Converters.Compressor) compressor (Turboprop attribute) (Turboshaft attribute) compressor_nondimensional_massflow (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) compute() (Cubic_Spline_Blender method) compute_absolute_viscosity() (Air method) (Glycol_Water method) (Steam method) compute_aft_centerbody_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_aft_centerbody_weight) compute_aircraft_moment_of_inertia() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_aircraft_moment_of_inertia) compute_airfoil_aerodynamics() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.BET_calculations), [1] compute_airfoil_properties() (in module RCAIDE.Library.Methods.Geometry.Airfoil.compute_airfoil_properties) compute_all() (Alcohol_Mixture method) (Alkane_Mixture method) compute_avionics_power_draw() (in module RCAIDE.Library.Methods.Powertrain.Systems.compute_avionics_power_draw), [1] compute_boom_fineness() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom), [1] compute_boom_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_boom_weight) compute_boundary_layer_properties() (in module RCAIDE.Library.Methods.Geometry.Airfoil.compute_airfoil_properties) compute_bus_conditions() (in module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.compute_bus_conditions) compute_cabin_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_cabin_weight) compute_chord_length_from_span_location() (in module RCAIDE.Library.Methods.Geometry.Planform.compute_chord_length_from_span_location) compute_coefficient() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.evaluate_VLM), [1] compute_coefficients() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.evaluate_VLM), [1] compute_combustor_performance() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_cantera) (in module RCAIDE.Library.Methods.Powertrain.Converters.Combustor.compute_combustor_performance) compute_component_centers_of_gravity() (in module RCAIDE.Library.Methods.Mass_Properties.Center_of_Gravity.compute_component_centers_of_gravity) compute_compression_nozzle_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Compression_Nozzle.compute_compression_nozzle_performance) compute_compressor_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Compressor.compute_compressor_performance) compute_constant_speed_internal_combustion_engine_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.compute_constant_speed_internal_combustion_engine_performance) compute_coolant_properties() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_rating_model) compute_cp() (Air method) (Glycol_Water method) (Steam method) compute_cuboid_moment_of_inertia() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_cuboid_moment_of_inertia) compute_current_in_from_throttle() (in module RCAIDE.Library.Methods.Powertrain.Modulators.Electronic_Speed_Controller.compute_esc_performance), [1] compute_cylinder_moment_of_inertia() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_cylinder_moment_of_inertia) compute_density() (Air method) (Glycol_Water method) (Steam method) compute_distributor_conditions() (Electrical_Bus method) compute_dR_dpsi() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] compute_ducted_fan_efficiency() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Rankine_Froude_Momentum_Theory.RFMT_performance) compute_ducted_fan_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.compute_ducted_fan_performance) compute_dynamic_flight_modes() (in module RCAIDE.Library.Methods.Stability.compute_dynamic_flight_modes) compute_electric_ducted_fan_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.compute_electric_ducted_fan_performance) compute_electric_rotor_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.compute_electric_rotor_performance) compute_engine_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight) compute_expansion_nozzle_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Expansion_Nozzle.compute_expansion_nozzle_performance) compute_extended_polars() (in module RCAIDE.Library.Methods.Geometry.Airfoil.compute_airfoil_properties) compute_fan_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fan.compute_fan_performance) compute_flap_lift() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_flap_lift) compute_fuel_cell_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_fuel_cell_performance) (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) compute_fuel_system_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_propulsion_system_weight) compute_fuselage_fineness() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] compute_fuselage_moment_of_inertia() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_fuselage_moment_of_inertia) compute_fuselage_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_fuselage_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_fuselage_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_fuselage_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_fuselage_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_fuselage_weight) compute_fusselage_dimensions() (in module RCAIDE.Library.Methods.Geometry.LOPA.compute_layout_of_passenger_accommodations) compute_G_1() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.LBL_VS_broadband_noise) compute_G_2() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.LBL_VS_broadband_noise) compute_G_3() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.LBL_VS_broadband_noise) compute_gamma() (Air method) (Steam method) compute_generator_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.compute_generator_performance) compute_gravity() (Earth method), [1] compute_heat_exchanger_performance() (Cross_Flow_Heat_Exchanger method) compute_heat_exhanger_factors() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.compute_heat_exhanger_factors) compute_heat_loss_to_environment() (in module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.compute_mixing_temperature) compute_horizontal_tail_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_horizontal_tail_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_horizontal_tail_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_horizontal_tail_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_horizontal_tail_weight) compute_induced_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.VLM) compute_inflow_and_tip_loss() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.BET_calculations), [1] compute_internal_combustion_engine_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.compute_internal_combustion_engine_performance) compute_jet_engine_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) compute_landing_gear_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_landing_gear_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_landing_gear_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_landing_gear_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_landing_gear_weight) compute_layout_of_passenger_accommodations() (in module RCAIDE.Library.Methods.Geometry.LOPA.compute_layout_of_passenger_accommodations) compute_lfp_cell_performance() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.compute_lfp_cell_performance) compute_lfp_cell_state() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.compute_lfp_cell_performance) compute_main_wing_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_main_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_main_wing_weight) compute_max_lift_coeff() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_max_lift_coeff) compute_misc_engine_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_propulsion_system_weight) compute_misc_propulsion_system_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight) compute_mixing_temperature() (in module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.compute_mixing_temperature) compute_mixture_density() (Alcohol_Mixture method) (Alkane_Mixture method) compute_mixture_energy_density() (Alcohol_Mixture method) (Alkane_Mixture method) compute_mixture_lower_heating_value() (Alcohol_Mixture method) (Alkane_Mixture method) compute_mixture_specific_energy() (Alcohol_Mixture method) (Alkane_Mixture method) compute_module_properties() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.compute_module_properties) compute_moment_of_inertia() (Blended_Wing_Body_Fuselage method) (Fuselage method) (Tube_Fuselage method) (Wing method) compute_motor_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.compute_motor_performance) compute_motor_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_motor_weight) compute_naca_4series() (in module RCAIDE.Library.Methods.Geometry.Airfoil.compute_naca_4series) compute_nacelle_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_propulsion_system_weight) compute_nmc_cell_performance() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.compute_nmc_cell_performance) compute_nmc_cell_state() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.compute_nmc_cell_performance) compute_noise_certification_data() (in module RCAIDE.Library.Methods.Performance.compute_noise_certification_data), [1] compute_operating_empty_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_operating_empty_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_operating_empty_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_operating_empty_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_operating_empty_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_operating_empty_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.General_Aviation.Physics_Based.compute_operating_empty_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_operating_empty_weight)

compute_operating_items_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_operating_items_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Common.compute_operating_items_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_operating_items_weight) compute_panel_area() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_VD_helpers), [1] compute_parasite_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_wing) compute_payload_power_draw() (in module RCAIDE.Library.Methods.Powertrain.Systems.compute_payload_power_draw), [1] compute_payload_range_diagram() (in module RCAIDE.Library.Methods.Performance.compute_payload_range_diagram) compute_payload_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Common.compute_payload_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_payload_weight) compute_performance() (Constant_Speed_Internal_Combustion_Engine method) (Electric_Ducted_Fan method) (Electric_Rotor method) (Internal_Combustion_Engine method) (Turboelectric_Generator method) (Turbofan method) (Turbojet method) (Turboprop method) (Turboshaft method) compute_piston_engine_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) compute_point_to_point_geospacial_data() (in module RCAIDE.Library.Methods.Geodesics.compute_point_to_point_geospacial_data) compute_power() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_power) (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.compute_power) compute_power_consumed() (Fan method) (Pump method) compute_power_difference() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_power_difference) compute_power_from_throttle() (in module RCAIDE.Library.Methods.Powertrain.Converters.Engine.compute_power_from_throttle) compute_prandtl_number() (Air method) (Glycol_Water method) compute_properties() (in module RCAIDE.Library.Methods.Mass_Properties.Center_of_Gravity.compute_component_centers_of_gravity) compute_propulsion_system_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_propulsion_system_weight) compute_R() (Air method) compute_R_c_0() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.LBL_VS_broadband_noise) compute_ram_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ram.compute_ram_performance) compute_reformer_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Reformer.compute_reformer_performance) compute_relative_noise_evaluation_locations() (in module RCAIDE.Library.Methods.Noise.Common.compute_relative_noise_evaluation_locations) compute_reservior_coolant_temperature() (Reservoir method) compute_RHS_matrix() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_RHS_matrix) compute_rotation_effects() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.VLM) compute_rotor_noise() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.compute_rotor_noise) compute_rotor_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.compute_rotor_performance) compute_rotor_point_source_coordinates() (in module RCAIDE.Library.Methods.Noise.Common.compute_noise_source_coordinates), [1] compute_rotor_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_rotor_weight) compute_slat_lift() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_slat_lift) compute_span_location_from_chord_length() (in module RCAIDE.Library.Methods.Geometry.Planform.compute_span_location_from_chord_length) compute_speed_of_sound() (Air method) (Steam method) compute_stability_derivative() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.evaluate_VLM), [1] compute_stack_properties() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Common.compute_stack_properties) compute_supersonic_nozzle_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Supersonic_Nozzle.compute_supersonic_nozzle_performance) compute_systems_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_systems_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_systems_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_systems_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_systems_weight) compute_thermal_conductivity() (Air method) (Glycol_Water method) compute_thermal_performance() (Air_Cooled method) (Liquid_Cooled_Wavy_Channel method) compute_throttle_from_power() (in module RCAIDE.Library.Methods.Powertrain.Converters.Engine.compute_throttle_from_power) compute_thrust() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.compute_thurst), [1] (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_thurst), [1] (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_thrust) compute_thrust_reverser_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight) compute_turbine_engine_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight) compute_turbine_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turbine.compute_turbine_performance) compute_turboelectric_generator_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.compute_turboelectric_generator_performance) compute_turbofan_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.compute_turbofan_performance) compute_turbojet_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_turbojet_performance) compute_turboprop_engine_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) compute_turboprop_performance() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_turboprop_performance) compute_turboshaft_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.compute_turboshaft_performance) compute_unit_normal() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_VD_helpers), [1] compute_values() (Atmospheric method) (Constant_Temperature method) (US_Standard_1976 method) compute_vehicle_center_of_gravity() (in module RCAIDE.Library.Methods.Mass_Properties.Center_of_Gravity.compute_vehicle_center_of_gravity) compute_vertical_tail_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_vertical_tail_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_vertical_tail_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_vertical_tail_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_vertical_tail_weight) compute_voltage() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_voltage) compute_voltage_out_from_throttle() (in module RCAIDE.Library.Methods.Powertrain.Modulators.Electronic_Speed_Controller.compute_esc_performance), [1] compute_wake_contraction_matrix() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.compute_wake_contraction_matrix) compute_wake_induced_velocity() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.compute_wake_induced_velocity) compute_wing_induced_velocity() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_wing_induced_velocity) compute_wing_moment_of_inertia() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_wing_moment_of_inertia) compute_wing_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_wing_weight) compute_wiring_weight() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_wiring_weight) concatenate_surfaces() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.airfoil_analysis) Conditions (class in RCAIDE.Framework.Mission.Common.Conditions) Conduction_laminar_flow (PMSM_Motor attribute) conductivity (Polyetherimide attribute) conductivity_electrical (Copper attribute) conductivity_thermal (Copper attribute) Config (class in RCAIDE.Library.Components.Configs.Config) configs_setup() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) Configuration (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Configuration) configuration_type (Control_Surface attribute) const_1 (Aluminum_Air.cell.ragone attribute) (Lithium_Sulfur.cell.ragone attribute) const_2 (Aluminum_Air.cell.ragone attribute) (Lithium_Sulfur.cell.ragone attribute) Constant_Acceleration_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude) Constant_Acceleration_Constant_Angle_Linear_Climb (class in RCAIDE.Framework.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb) Constant_Acceleration_Constant_Pitchrate_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude) Constant_CAS_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_CAS_Constant_Rate) (class in RCAIDE.Framework.Mission.Segments.Descent.Constant_CAS_Constant_Rate) Constant_Dynamic_Pressure_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude) Constant_Dynamic_Pressure_Constant_Altitude_Loiter (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter) Constant_Dynamic_Pressure_Constant_Angle (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle) Constant_Dynamic_Pressure_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate) Constant_EAS_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_EAS_Constant_Rate) (class in RCAIDE.Framework.Mission.Segments.Descent.Constant_EAS_Constant_Rate) Constant_Mach_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude) Constant_Mach_Constant_Altitude_Loiter (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter) Constant_Mach_Constant_Angle (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Constant_Angle) Constant_Mach_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Constant_Rate) Constant_Mach_Linear_Altitude (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Linear_Altitude) Constant_Pitch_Rate_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude) Constant_Speed_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude) Constant_Speed_Constant_Altitude_Loiter (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter) Constant_Speed_Constant_Angle (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Constant_Angle) (class in RCAIDE.Framework.Mission.Segments.Descent.Constant_Speed_Constant_Angle) Constant_Speed_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Constant_Rate) (class in RCAIDE.Framework.Mission.Segments.Descent.Constant_Speed_Constant_Rate) Constant_Speed_Internal_Combustion_Engine (class in RCAIDE.Library.Components.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine) Constant_Speed_Linear_Altitude (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Linear_Altitude) Constant_Temperature (class in RCAIDE.Framework.Analyses.Atmospheric.Constant_Temperature) (class in RCAIDE.Library.Attributes.Atmospheres.Earth.Constant_Temperature) Constant_Throttle_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude) Constant_Throttle_Constant_Speed (class in RCAIDE.Framework.Mission.Segments.Climb.Constant_Throttle_Constant_Speed) Constants (class in RCAIDE.Library.Methods.Geodesics.Geodesics), [1] constraints_individual() (Nexus method) Container (class in RCAIDE.Framework.Analyses.Analysis) (class in RCAIDE.Framework.Core.Container) (class in RCAIDE.Framework.Core.Diffed_Data) (class in RCAIDE.Framework.Mission.Common.State) (class in RCAIDE.Framework.Mission.Segments.Segment) (class in RCAIDE.Framework.Mission.Sequential_Segments) (class in RCAIDE.Framework.Networks.Network) (class in RCAIDE.Library.Components.Booms.Boom) (class in RCAIDE.Library.Components.Component) (class in RCAIDE.Library.Components.Network) (class in RCAIDE.Library.Components.Wings.Wing) (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Run_Case) ContainerOrdered (class in RCAIDE.Framework.Core.ContainerOrdered) contour_surface_slice() (in module RCAIDE.Library.Plots.Geometry.Common.contour_surface_slice) control (System attribute) Control_Surface (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Control_Surface) (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing) Control_Surface_Data (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing) control_surface_deflection_command() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) Control_Surface_Results (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing) control_surfaces (Wing attribute) control_surfaces() (in module RCAIDE.Library.Mission.Common.Unpack_Unknowns.control_surfaces) Convection_laminar_flow (PMSM_Motor attribute) convective_heat_transfer_coefficient (Air_Cooled attribute) Conventional (class in RCAIDE.Framework.Analyses.Weights.Conventional) conventional_payload_range_diagram() (in module RCAIDE.Library.Methods.Performance.compute_payload_range_diagram) converge() (in module RCAIDE.Library.Mission.Solver.converge) (Segment method) conversion_efficiency (Turboshaft attribute) convert_airfoil_to_meshgrid() (in module RCAIDE.Library.Methods.Geometry.Airfoil.convert_airfoil_to_meshgrid) convert_keas() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) convert_sweep() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing), [1] (in module RCAIDE.Library.Methods.Geometry.Planform.convert_sweep) convert_sweep_segments() (in module RCAIDE.Library.Methods.Geometry.Planform.convert_sweep) convert_to_segmented_wing() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) convert_to_third_octave_band() (in module RCAIDE.Library.Methods.Noise.Common.convert_to_third_octave_band) convert_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] Converter (class in RCAIDE.Library.Components.Powertrain.Converters.Converter) Coolant (class in RCAIDE.Library.Attributes.Coolants.Coolant) coolant (Cross_Flow_Heat_Exchanger attribute) (Reservoir attribute) coolant_hydraulic_diameter (Cross_Flow_Heat_Exchanger attribute) Coolant_Line (class in RCAIDE.Library.Components.Powertrain.Distributors.Coolant_Line) cooling_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.cooling_drag) cooling_fluid (Air_Cooled attribute) coordinate_file (Airfoil attribute) Copper (class in RCAIDE.Library.Attributes.Materials.Copper) copy_data_from_paths() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) copy_large_container() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) copy_wings() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) core_nozzle (Turbofan attribute) (Turbojet attribute) (Turboshaft attribute) Correlation_Buildup (class in RCAIDE.Framework.Analyses.Noise.Correlation_Buildup) cowling_airfoil_angle (Nacelle attribute) Cp_polynomial_coefficients (Ducted_Fan attribute) create_class_seating_map_layout() (in module RCAIDE.Library.Methods.Geometry.LOPA.compute_layout_of_passenger_accommodations) create_discharge_performance_map() (in module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_LFP) (in module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_NMC) Cross_Flow_Heat_Exchanger (class in RCAIDE.Library.Components.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger) cross_flow_heat_exchanger_geometry_setup() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_geometry_setup) cross_flow_heat_exchanger_sizing_setup() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_sizing_setup) cross_flow_hex_rating_model() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_hex_rating_model) crossflow_heat_exchanger_design_problem_setup() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.design_cross_flow_heat_exchanger) CrossLinked_Polyethylene (class in RCAIDE.Library.Attributes.Materials.CrossLinked_Polyethylene) cruise (Ducted_Fan attribute) (Prop_Rotor attribute) Cryogen (class in RCAIDE.Library.Attributes.Cryogens.Cryogen) cryogenic (Cryogenic_Tank attribute) cryogenic_selector_ratio (Cryogenic_Tank attribute) Cryogenic_Tank (class in RCAIDE.Library.Components.Powertrain.Sources.Cryogenic_Tanks.Cryogenic_Tank) Ct_polynomial_coefficients (Ducted_Fan attribute) Cubic_Spline_Blender (class in RCAIDE.Library.Methods.Utilities.Cubic_Spline_Blender) current_capacitor_charge (Generic_Battery_Module attribute) current_energy (Generic_Battery_Module attribute) curvature (Ellipse_Segment attribute) (Segment attribute), [1] Curved_Constant_Radius_Constant_Speed_Constant_Altitude (class in RCAIDE.Framework.Mission.Segments.Cruise.Curved_Constant_Radius_Constant_Speed_Constant_Altitude) curvilinear_inertial_horizontal_position() (in module RCAIDE.Library.Mission.Common.Update.curvilinear_inertial_horizontal_position)

D

Data (class in RCAIDE.Framework.Core.Data) (Vehicle attribute) dataname() (Data method) (DataOrdered method) DataOrdered (class in RCAIDE.Framework.Core.DataOrdered) DC_Generator (class in RCAIDE.Library.Components.Powertrain.Converters.DC_Generator) DC_Motor (class in RCAIDE.Library.Components.Powertrain.Converters.DC_Motor) deep_get() (Data method) (DataOrdered method) deep_set() (Data method) (DataOrdered method) deflect_control_surface() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1] deflect_control_surface_strip() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1] deflect_control_surfaces() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1] deflection (All_Moving_Surface attribute) (Control_Surface attribute) Delta_T (PMSM_Motor attribute) density (Acrylic attribute) (Alcohol_Mixture attribute) (Alkane_Mixture attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Aviation_Gasoline attribute) (Bidirectional_Carbon_Fiber attribute) (Butanol attribute) (Carbon_Fiber_Honeycomb attribute) (Coolant attribute) (Copper attribute) (Cross_Flow_Heat_Exchanger attribute) (CrossLinked_Polyethylene attribute) (Cryogen attribute) (Epoxy attribute) (Ethane attribute) (Ethanol attribute) (Gaseous_Hydrogen attribute) (Glycol_Water attribute) (Jet_A attribute) (Jet_A1 attribute) (JP7 attribute) (Liquid_Hydrogen attribute), [1] (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Magnesium attribute) (Methane attribute) (Nickel attribute) (Paint attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) (Propane attribute) (Propanol attribute) (Propellant attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute) density_of_fluid (PMSM_Motor attribute) Descent (class in RCAIDE.Framework.Mission.Segments.Vertical_Flight.Descent) design_altitude (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) design_constant_speed_internal_combustion_engine() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.design_constant_speed_internal_combustion_engine) design_cross_flow_heat_exchanger() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.design_cross_flow_heat_exchanger) design_ducted_fan() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.design_ducted_fan) design_electric_ducted_fan() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.design_electric_ducted_fan) design_electric_rotor() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.design_electric_rotor)

design_heat_removed (Cross_Flow_Heat_Exchanger attribute) design_internal_combustion_engine() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.design_internal_combustion_engine) design_isa_deviation (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) design_lift_rotor() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_lift_rotor) design_mach_number (Turboprop attribute) design_mass_flow_rate (Turbofan attribute) (Turbojet attribute) (Turboshaft attribute) design_optimal_generator() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator) design_optimal_motor() (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor) design_power (Turboshaft attribute) design_prop_rotor() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_prop_rotor) design_propeller() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_propeller) design_thrust (Turbofan attribute) (Turbojet attribute) design_torque (DC_Generator attribute) (DC_Motor attribute) (PMSM_Generator attribute) design_turboelectric_generator() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.design_turboelectric_generator) design_turbofan() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.design_turbofan) design_turbojet() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.design_turbojet) design_turboprop() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.design_turboprop) design_turboshaft() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.design_turboshaft) design_wavy_channel() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.design_wavy_channel) destination() (Distance method), [1] determine_fuselage_chord() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) diameter (Combustor attribute) (Nacelle attribute) (Turbofan attribute) (Turboprop attribute) (Turboshaft attribute) dictgetitem() (in module RCAIDE.Framework.Core.Data) dielectric_strength_range (CrossLinked_Polyethylene attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) diff() (in module RCAIDE.Framework.Core.Diffed_Data) Diffed_Data (class in RCAIDE.Framework.Core.Diffed_Data) Diffed_Data.Container (class in RCAIDE.Framework.Core.Diffed_Data) differential_pressure (Boom attribute) (Fuselage attribute) (Nacelle attribute) differentials_altitude() (in module RCAIDE.Library.Mission.Common.Initialize.differentials_altitude) differentials_dimensionless() (in module RCAIDE.Library.Mission.Common.Initialize.differentials_dimensionless) differentials_time() (in module RCAIDE.Library.Mission.Common.Update.differentials_time) dihedral (Wing attribute) dihedral_outboard (Segment attribute) Distance (class in RCAIDE.Library.Methods.Geodesics.Geodesics), [1] DISTANCE (Geodesic attribute), [1] (GeodesicCapability attribute), [1] distance (in module RCAIDE.Library.Methods.Geodesics.Geodesics), [1] DISTANCE_IN (Geodesic attribute), [1] (GeodesicCapability attribute), [1] drag_divergence() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.drag_divergence) duct_vel_to_body() (Ducted_Fan method) ducted (Rotor attribute) Ducted_Fan (class in RCAIDE.Library.Components.Powertrain.Converters.Ducted_Fan) ducted_fan (Electric_Ducted_Fan attribute) Ducted_Fan_Design_Code (class in RCAIDE.Framework.Analyses.Propulsion.Ducted_Fan_Design_Code) dynamic_pressure_ratio (Wing attribute) dynamic_viscosity (Coolant attribute) (Glycol_Water attribute) dynamo_supply_mass_estimation() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.dynamo_supply_mass_estimation)

E

Earth (class in RCAIDE.Framework.Analyses.Planets.Earth) (class in RCAIDE.Library.Attributes.Planets.Earth) Economy (class in RCAIDE.Library.Components.Fuselages.Cabins.Classes.Economy) effective_diameter (Boom attribute) (Fuselage attribute) efficiency (Coolant_Line attribute) (DC_Generator attribute) (DC_Motor attribute) (Electrical_Bus attribute) (Electronic_Speed_Controller attribute) (Fan attribute) (Fuel_Line attribute) (Fuel_Selector attribute) (PMSM_Generator attribute) (Pump attribute) (Turboprop.gearbox attribute) Electric (class in RCAIDE.Framework.Analyses.Weights.Electric) (class in RCAIDE.Framework.Networks.Electric) Electric_Ducted_Fan (class in RCAIDE.Library.Components.Powertrain.Propulsors.Electric_Ducted_Fan) electric_payload_range_diagram() (in module RCAIDE.Library.Methods.Performance.compute_payload_range_diagram) Electric_Rotor (class in RCAIDE.Library.Components.Powertrain.Propulsors.Electric_Rotor) Electrical_Bus (class in RCAIDE.Library.Components.Powertrain.Distributors.Electrical_Bus) electrical_conductivity() (Copper method) electrical_configuration (Generic_Battery_Module attribute) electrical_permittivity (CrossLinked_Polyethylene attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) Electronic_Speed_Controller (class in RCAIDE.Library.Components.Powertrain.Modulators.Electronic_Speed_Controller) electronic_speed_controller (Electric_Ducted_Fan attribute) (Electric_Rotor attribute) Elevator (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Elevator) Ellipse_Segment (class in RCAIDE.Library.Components.Fuselages.Segments.Ellipse_Segment) Emission_Index_Correlation_Method (class in RCAIDE.Framework.Analyses.Emissions.Emission_Index_Correlation_Method) Emission_Index_CRN_Method (class in RCAIDE.Framework.Analyses.Emissions.Emission_Index_CRN_Method) emission_indices (Jet_A attribute) (Jet_A1 attribute) (Propellant attribute) Emissions (class in RCAIDE.Framework.Analyses.Emissions.Emissions) emissions() (in module RCAIDE.Library.Mission.Common.Pre_Process.emissions) (in module RCAIDE.Library.Mission.Common.Update.emissions) emissivity (Polyetherimide attribute) EMPTY (Geodesic attribute), [1] (GeodesicCapability attribute), [1] empty_mass (Central_Fuel_Tank.mass_properties attribute) (Cryogenic_Tank.mass_properties attribute) (Fuel_Tank.mass_properties attribute) (Wing_Fuel_Tank.mass_properties attribute) Energy (class in RCAIDE.Framework.Analyses.Energy.Energy) energy() (in module RCAIDE.Library.Mission.Common.Initialize.energy) (in module RCAIDE.Library.Mission.Common.Pre_Process.energy) (in module RCAIDE.Library.Mission.Common.Update.energy) energy_balance() (in module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.compute_mixing_temperature) energy_calc() (Generic_Fuel_Cell_Stack method) (Lithium_Ion_LFP method) (Lithium_Ion_NMC method) (Proton_Exchange_Membrane_Fuel_Cell method) energy_density (Alcohol_Mixture attribute) (Alkane_Mixture attribute) (Butanol attribute) (Cryogen attribute) (Ethane attribute) (Ethanol attribute) (Gaseous_Hydrogen attribute) (Generic_Battery_Module attribute) (Jet_A attribute) (Jet_A1 attribute) (JP7 attribute) (Liquid_Hydrogen attribute), [1] (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Methane attribute) (Propane attribute) (Propanol attribute) (Propellant attribute) Engine (class in RCAIDE.Library.Components.Powertrain.Converters.Engine)

engine (Constant_Speed_Internal_Combustion_Engine attribute) (Internal_Combustion_Engine attribute) EPNL_noise_metric() (in module RCAIDE.Library.Methods.Noise.Metrics.EPNL_noise_metric) Epoxy (class in RCAIDE.Library.Attributes.Materials.Epoxy) equality_constraint() (Nexus method) equation() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_sizing_setup) Equivalent_SENEL_SEL_noise_metrics() (in module RCAIDE.Library.Methods.Noise.Metrics.Equivalent_SENEL_SEL_noise_metrics) estimate_2ndseg_lift_drag_ratio() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.estimate_2ndseg_lift_drag_ratio) estimate_landing_field_length() (in module RCAIDE.Library.Methods.Performance.estimate_landing_field_length) estimate_stall_speed() (in module RCAIDE.Library.Methods.Performance.estimate_stall_speed) estimate_take_off_field_length() (in module RCAIDE.Library.Methods.Performance.estimate_take_off_field_length) estimate_wing_internal_volume() (in module RCAIDE.Library.Methods.Geometry.Planform.estimate_wing_internal_volume), [1] eta (Reformer attribute) eta_transform() (Cubic_Spline_Blender method) etap_polynomial_coefficients (Ducted_Fan attribute) Ethane (class in RCAIDE.Library.Attributes.Propellants.Ethane) Ethanol (class in RCAIDE.Library.Attributes.Propellants.Ethanol) evalaute_aircraft() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) Evaluate (class in RCAIDE.Framework.Mission.Segments.Evaluate), [1] evaluate() (Aerodynamics method) (Analysis method) (Analysis.Container method) (Athena_Vortex_Lattice method), [1] (Container method), [1], [2] (Emission_Index_Correlation_Method method) (Emission_Index_CRN_Method method) (Emissions method) (Energy method) (Network method) (Network.Container method) (Nexus method) (Noise method) (Process method) (Process_Geometry method) (Segment method) (Sequential_Segments method) (Sequential_Segments.Container method) (Vortex_Lattice_Method method), [1] (Weights method) evaluate_AVL_no_surrogate() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.evaluate_AVL), [1] evaluate_AVL_surrogate() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.evaluate_AVL), [1] evaluate_cantera() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_cantera) evaluate_CEM() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) evaluate_constraints() (Trust_Region_Optimization method), [1] evaluate_corrected_model() (Additive_Solver method), [1] (Trust_Region_Optimization method), [1] evaluate_correlation_emissions_indices() (in module RCAIDE.Library.Methods.Emissions.Emission_Index_Empirical_Method.evaluate_correlation_emissions_indices) evaluate_CRN_emission_indices_no_surrogate() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_CRN_emission_indices), [1] evaluate_CRN_emission_indices_surrogate() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_CRN_emission_indices), [1] evaluate_expected_improvement() (Additive_Solver method), [1] evaluate_function() (Trust_Region method), [1] evaluate_max_gross_power() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) evaluate_model() (Additive_Solver method), [1] (Trust_Region_Optimization method), [1] evaluate_no_surrogate() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.evaluate_VLM), [1] evaluate_noise() (Correlation_Buildup method) (Frequency_Domain_Buildup method) evaluate_PEM() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) evaluate_power_func() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) evaluate_slipstream() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] evaluate_surrogate() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.evaluate_VLM), [1] evaluate_wake() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] evaluate_wake_velocities() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] exa (Turbofan attribute) exit_radius (Ducted_Fan attribute) expand_rows() (Conditions method) (State method) expand_state() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise), [1] (in module RCAIDE.Library.Mission.Solver.expand_state) expanded_array (class in RCAIDE.Framework.Mission.Common.Conditions) Expansion_Nozzle (class in RCAIDE.Library.Components.Powertrain.Converters.Expansion_Nozzle) export_vsp_vehicle() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.export_vsp_vehicle) exposed_root_chord_offset (Wing attribute) extend() (Container method) external_plug_effect() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.external_plug_effect), [1] extract_wing_collocation_points() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.extract_wing_collocation_points)

F

f (Geodesic attribute), [1] f_air_PZ (Combustor attribute) F_SC (Combustor attribute) Fan (class in RCAIDE.Library.Components.Powertrain.Converters.Fan) (class in RCAIDE.Library.Components.Thermal_Management.Accessories.Fan) fan (Turbofan attribute) fan_effectiveness (Ducted_Fan attribute) fan_nozzle (Turbofan attribute) FAR_st (Combustor attribute) fidelity (Ducted_Fan attribute) fin_area_density_cold (Cross_Flow_Heat_Exchanger attribute) fin_area_density_hot (Cross_Flow_Heat_Exchanger attribute) fin_conductivity (Cross_Flow_Heat_Exchanger attribute) fin_exposed_strip_edge_cold (Cross_Flow_Heat_Exchanger attribute) fin_exposed_strip_edge_hot (Cross_Flow_Heat_Exchanger attribute) fin_metal_thickness_cold (Cross_Flow_Heat_Exchanger attribute) fin_metal_thickness_hot (Cross_Flow_Heat_Exchanger attribute) fin_spacing_cold (Cross_Flow_Heat_Exchanger attribute) fin_spacing_hot (Cross_Flow_Heat_Exchanger attribute) find_a_star() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] find_aluminum_mass() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Aluminum_Air.compute_al_air_cell_performance), [1] find_component_root() (Vehicle method) find_energy_network_root() (Vehicle method) find_fuse_u_coordinate() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom), [1] (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] find_mass_gain_rate() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_mass_gain_rate) find_ragone_properties() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_ragone_properties) find_specific_power() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_specific_power) find_sweep() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) find_take_off_weight_given_tofl() (in module RCAIDE.Library.Methods.Performance.find_take_off_weight_given_tofl) find_total_mass_gain() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_total_mass_gain) find_water_mass() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Aluminum_Air.compute_al_air_cell_performance), [1] fineness (Boom attribute) (Fuselage attribute) finite_difference() (Nexus method) finned_area_to_total_area_cold (Cross_Flow_Heat_Exchanger attribute) finned_area_to_total_area_hot (Cross_Flow_Heat_Exchanger attribute) First (class in RCAIDE.Library.Components.Fuselages.Cabins.Classes.First) FixPointNormalize (class in RCAIDE.Library.Plots.Noise.plot_2D_noise_contour) (class in RCAIDE.Library.Plots.Topography.plot_elevation_contours) Flap (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Flap) flap_angle (Rotor attribute) flat_rate_altitude (Engine attribute) flatten_matrix() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.broadband_noise) flight_dynamics() (in module RCAIDE.Library.Mission.Common.Residuals.flight_dynamics) flight_dynamics_and_controls() (Segment method) flip_1() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1]

flip_2() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1] flow_through (Nacelle attribute) flowspeed (Air_Cooled.cooling_fluid attribute) fluid_properties (Constant_Temperature attribute) (US_Standard_1976 attribute) fm_id() (in module RCAIDE.Library.Methods.Gas_Dynamics.fm_id) folder (class in RCAIDE.Framework.Core.redirect), [1] forces() (in module RCAIDE.Library.Mission.Common.Update.forces) freestream() (in module RCAIDE.Library.Mission.Common.Update.freestream) Frequency_Domain_Buildup (class in RCAIDE.Framework.Analyses.Noise.Frequency_Domain_Buildup) fuel (Central_Fuel_Tank attribute) Fuel (class in RCAIDE.Framework.Networks.Fuel) fuel (Fuel_Tank attribute) (Wing_Fuel_Tank attribute) Fuel_Cell (class in RCAIDE.Framework.Networks.Fuel_Cell) fuel_chemical_properties (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Jet_A attribute) (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Methane attribute) (Propane attribute) (Propanol attribute) fuel_equivalency_ratio (Combustor attribute) Fuel_Line (class in RCAIDE.Library.Components.Powertrain.Distributors.Fuel_Line) Fuel_Selector (class in RCAIDE.Library.Components.Powertrain.Modulators.Fuel_Selector) fuel_selector_ratio (Central_Fuel_Tank attribute) (Fuel_Tank attribute) (Wing_Fuel_Tank attribute) fuel_surrogate_chemical_properties (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Jet_A attribute) (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Methane attribute) (Propane attribute) (Propanol attribute) Fuel_Tank (class in RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks.Fuel_Tank) fuel_tanks (Fuel_Line attribute) (Fuselage attribute) (Wing attribute) fuel_velocity_ratio (Combustor attribute) Fuselage (class in RCAIDE.Library.Components.Fuselages.Fuselage) fuselage_correction() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.fuselage_correction) fuselage_planform() (in module RCAIDE.Library.Methods.Geometry.Planform.fuselage_planform) fw() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.wave_drag)

G

gain (Control_Surface attribute) Gas (class in RCAIDE.Library.Attributes.Gases.Gas) gas_constant (Gaseous_Hydrogen attribute) gas_cp_coefficients (Liquid_Hydrogen attribute) gas_specific_constant (Air attribute) (CO2 attribute) (Gas attribute) (Rocket_LH2 attribute) (Rocket_RP1 attribute) (Steam attribute) Gaseous_Hydrogen (class in RCAIDE.Library.Attributes.Propellants.Gaseous_Hydrogen) gear_extended (Landing_Gear attribute) gear_ratio (DC_Generator.gearbox attribute) (DC_Motor.gearbox attribute) (PMSM_Generator.gearbox attribute) gearbox (Turboelectric_Generator attribute) generate_3d_basic_nacelle_points() (in module RCAIDE.Library.Plots.Geometry.plot_3d_nacelle) generate_3d_blade_points() (in module RCAIDE.Library.Plots.Geometry.plot_3d_rotor) generate_3d_BOR_nacelle_points() (in module RCAIDE.Library.Plots.Geometry.plot_3d_nacelle) generate_3d_fuselage_points() (in module RCAIDE.Library.Plots.Geometry.plot_3d_fuselage), [1] generate_3d_stack_nacelle_points() (in module RCAIDE.Library.Plots.Geometry.plot_3d_nacelle) generate_3d_vehicle_geometry_data() (in module RCAIDE.Library.Plots.Geometry.plot_3d_vehicle) generate_3d_wing_points() (in module RCAIDE.Library.Plots.Geometry.plot_3d_wing) generate_fuselage_and_nacelle_vortex_distribution() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_vortex_distribution) generate_hemisphere_microphone_locations() (in module RCAIDE.Library.Methods.Noise.Common.generate_hemisphere_microphone_locations) generate_int_stations() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) generate_interpolated_airfoils() (in module RCAIDE.Library.Methods.Geometry.Airfoil.generate_interpolated_airfoils), [1] generate_terrain_microphone_locations() (in module RCAIDE.Library.Methods.Noise.Common.generate_terrain_microphone_locations) generate_V_n_diagram() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) generate_vortex_distribution() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_vortex_distribution) generate_wing_stations() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) generate_wing_vortex_distribution() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_vortex_distribution) generate_zero_elevation_microphone_locations() (in module RCAIDE.Library.Methods.Noise.Common.generate_zero_elevation_microphone_locations) generator (Turboelectric_Generator attribute) Generic_Battery_Module (class in RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Generic_Battery_Module) Generic_Fuel_Cell_Stack (class in RCAIDE.Library.Components.Powertrain.Converters.Generic_Fuel_Cell_Stack) Geodesic (class in RCAIDE.Library.Methods.Geodesics.Geodesics), [1] Geodesic_Calculate (class in RCAIDE.Library.Methods.Geodesics.Geodesics), [1] GeodesicCapability (class in RCAIDE.Library.Methods.Geodesics.Geodesics), [1] GeodesicDistance (in module RCAIDE.Library.Methods.Geodesics.Geodesics), [1] GEODESICSCALE (Geodesic attribute), [1] (GeodesicCapability attribute), [1] GEOGRAPHICLIB_GEODESIC_ORDER (Geodesic attribute), [1] geometrtic_configuration (Generic_Battery_Module attribute) geometry (Airfoil attribute)

geometry_Ce (Turbofan attribute) geometry_key (Process_Geometry attribute) geometry_xe (Turbofan attribute) geometry_ye (Turbofan attribute) get() (DataOrdered method) get_bases() (Data method) (DataOrdered method) get_boom_height() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom), [1] get_children() (Airfoil_Container method) (Container method) (ContainerOrdered method) (Segment_Container method), [1], [2], [3] (Wing.Container method) get_fuel_tank_properties() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.get_fuel_tank_properties) get_fuel_tanks() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.get_fuel_tank_properties) get_fuselage_height() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] get_paths() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) get_root() (Vehicle method) get_seat_x_coords() (in module RCAIDE.Library.Methods.Geometry.LOPA.LOPA_functions), [1] get_seat_y_coords() (in module RCAIDE.Library.Methods.Geometry.LOPA.LOPA_functions), [1] get_spanwise_engine() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) get_tags() (in module RCAIDE.Framework.Core.Container) get_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] get_vsp_measurements() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.get_vsp_measurements) get_vsp_trim_from_RCAIDE_trim() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing), [1] getcf() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method) getH() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method) global_warming_potential_100 (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Jet_A attribute) (Jet_A1 attribute) (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Methane attribute) (Propane attribute) (Propanol attribute) (Propellant attribute) Glycol_Water (class in RCAIDE.Library.Attributes.Coolants.Glycol_Water) gravity() (in module RCAIDE.Library.Mission.Common.Update.gravity) Ground (class in RCAIDE.Framework.Mission.Segments.Ground.Ground) ground() (in module RCAIDE.Library.Mission.Common.Unpack_Unknowns.ground) ground_forces() (in module RCAIDE.Library.Mission.Common.Update.ground_forces) ground_proximity_effect() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.ground_proximity_effect), [1] gust_dive_speed_intersection() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) gust_loads() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram)

H

hard_constraint_1() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator) (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor) hard_constraint_2() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator) (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor) harmonic_noise_line() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.harmonic_noise_line) harmonic_noise_plane() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.harmonic_noise_plane) harmonic_noise_point() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.harmonic_noise_point) has_key() (DataOrdered method) has_pylon (Nacelle attribute) hasattr() (DataOrdered method) heads_method() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.heads_method) heat_exchanger_efficiency (Cross_Flow_Heat_Exchanger attribute) heat_exchangers (Coolant_Line attribute) heat_transfer_efficiency (Air_Cooled attribute) height (Central_Fuel_Tank attribute) (Circle_Segment attribute) (Ellipse_Segment attribute) (Generic_Battery_Module attribute) (Reservoir attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute) (Turbofan attribute) (Turboprop attribute) (Turboshaft attribute) (Wing_Fuel_Tank attribute) height_of_duct (PMSM_Motor attribute) heights (Boom attribute) (Fuselage attribute)

hess_smith() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.hess_smith) high_lift (Wing attribute) high_mach (Wing attribute) high_pressure_compressor (Turbofan attribute) (Turbojet attribute) high_pressure_turbine (Turbofan attribute) (Turbojet attribute) (Turboshaft attribute) hinge_fraction (Aileron attribute) (All_Moving_Surface attribute) (Control_Surface attribute) (Elevator attribute) (Flap attribute) (Rudder attribute) (Slat attribute) hinge_vector (All_Moving_Surface attribute) Horizontal_Tail (class in RCAIDE.Library.Components.Wings.Horizontal_Tail) horizontal_tail_planform() (in module RCAIDE.Library.Methods.Geometry.Planform.horizontal_tail_planform) horizontal_tail_planform_raymer() (in module RCAIDE.Library.Methods.Geometry.Planform.horizontal_tail_planform_raymer) Hover (class in RCAIDE.Framework.Mission.Segments.Vertical_Flight.Hover) hover (Lift_Rotor attribute) (Prop_Rotor attribute) hub_radius (Ducted_Fan attribute) (Rotor attribute) Hybrid (class in RCAIDE.Framework.Analyses.Weights.Hybrid) (class in RCAIDE.Framework.Networks.Hybrid) hydraulic_diameter_of_duct (PMSM_Motor attribute) Hydrogen (class in RCAIDE.Framework.Analyses.Weights.Hydrogen)

I

identical_battery_modules (Coolant_Line attribute) (Electrical_Bus attribute) import_airfoil_dat() (in module RCAIDE.Library.Methods.Geometry.Airfoil.import_airfoil_dat) import_airfoil_geometry() (in module RCAIDE.Library.Methods.Geometry.Airfoil.import_airfoil_geometry) import_airfoil_polars() (in module RCAIDE.Library.Methods.Geometry.Airfoil.import_airfoil_polars) import_vsp_vehicle() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.import_vsp_vehicle) induced_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.induced_drag) induced_power_factor (Rotor attribute) inequality_constraint() (Nexus method) inertial_position() (in module RCAIDE.Library.Mission.Common.Initialize.inertial_position) infl_coeff() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.infl_coeff) initialize() (Analysis method) (Analysis.Container method) (Athena_Vortex_Lattice method), [1] (Container method) (Emission_Index_Correlation_Method method) (Emission_Index_CRN_Method method) (Segment method) (Vortex_Lattice_Method method), [1] initialize_bus_properties() (Electrical_Bus method) (in module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.initialize_bus_properties) initialize_conditions() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_CAS_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_EAS_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Angle), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Linear_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Linear_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Linear_Mach_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Linear_Speed_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Cruise.Curved_Constant_Radius_Constant_Speed_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Descent.Constant_CAS_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Descent.Constant_EAS_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Descent.Constant_Speed_Constant_Angle), [1] (in module RCAIDE.Library.Mission.Segments.Descent.Constant_Speed_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Descent.Linear_Mach_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Descent.Linear_Speed_Constant_Rate), [1] (in module RCAIDE.Library.Mission.Segments.Ground.Battery_Charge_Discharge), [1] (in module RCAIDE.Library.Mission.Segments.Ground.Landing), [1] (in module RCAIDE.Library.Mission.Segments.Ground.Takeoff), [1] (in module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_AVL_Trimmed), [1] (in module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion), [1] (in module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Throttle), [1] (in module RCAIDE.Library.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb), [1] (in module RCAIDE.Library.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Untrimmed.Untrimmed), [1] (in module RCAIDE.Library.Mission.Segments.Vertical_Flight.Climb), [1] (in module RCAIDE.Library.Mission.Segments.Vertical_Flight.Descent), [1] (in module RCAIDE.Library.Mission.Segments.Vertical_Flight.Hover), [1]

initialize_conditions_unpack_unknowns() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle), [1] initialize_opt_vals() (Additive_Solver method), [1] initialize_opt_vals_SHGO() (Additive_Solver method), [1] initialize_opt_vals_SLSQP() (Additive_Solver method), [1] initialize_SLSQP_constraints() (Trust_Region_Optimization method), [1] inlet_diameter (Nacelle attribute) inlet_nozzle (Turbofan attribute) (Turbojet attribute) (Turboshaft attribute) Inputs (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Inputs) inputs (Network attribute) integrate_velocity() (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude), [1] integrated_propulsion_jet() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) integrated_propulsion_piston() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight) Internal_Combustion_Engine (class in RCAIDE.Library.Components.Powertrain.Propulsors.Internal_Combustion_Engine) interp2d() (in module RCAIDE.Framework.Core.Utilities), [1] interpolate (Copper attribute) interpolated_func (DC_Generator attribute) (DC_Motor attribute) (PMSM_Generator attribute) Inverse() (Geodesic method), [1] inverse_calculation (Turboelectric_Generator attribute) isentropic_expansion_factor (Rocket_LH2 attribute) (Rocket_RP1 attribute) items() (DataOrdered method) iterate() (Segment method) iterate_optimizer() (in module RCAIDE.Library.Mission.Solver.converge) iterate_root_finder() (in module RCAIDE.Library.Mission.Solver.converge) iterate_segment() (in module RCAIDE.Library.Mission.Solver.converge) iteration() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] iterkeys() (DataOrdered method)

J

Jet_A (class in RCAIDE.Library.Attributes.Propellants.Jet_A) Jet_A1 (class in RCAIDE.Library.Attributes.Propellants.Jet_A1)

jet_installation_effect() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.jet_installation_effect), [1] JP7 (class in RCAIDE.Library.Attributes.Propellants.JP7)

K

keys() (DataOrdered method) kilometers (Distance property), [1]

kinematic_viscosity (Glycol_Water attribute) kinematics() (in module RCAIDE.Library.Mission.Common.Update.kinematics) km (Distance property), [1]

L

L_PZ (Combustor attribute) L_SZ (Combustor attribute) Landing (class in RCAIDE.Framework.Mission.Segments.Ground.Landing) Landing_Gear (class in RCAIDE.Library.Components.Landing_Gear.Landing_Gear) landing_gear_noise() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.landing_gear_noise) LatFix() (Math static method), [1] latin_hypercube_sampling() (in module RCAIDE.Library.Methods.Utilities.latin_hypercube_sampling) LATITUDE (Geodesic attribute), [1] (GeodesicCapability attribute), [1] LBL_VS_broadband_noise() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.LBL_VS_broadband_noise) length (Central_Fuel_Tank attribute) (Combustor attribute) (Ducted_Fan attribute) (Generic_Battery_Module attribute) (Nacelle attribute) (Reservoir attribute) (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) (Wing_Fuel_Tank attribute) length_of_channel (PMSM_Motor attribute) length_of_conductive_path (PMSM_Motor attribute) length_of_path (PMSM_Motor attribute) lengths (Boom attribute) (Fuselage attribute) LHV_CO (Reformer attribute) LHV_F (Reformer attribute) LHV_H2 (Reformer attribute) lift_equivalent_area() (in module RCAIDE.Library.Methods.Noise.Boom.lift_equivalent_area), [1] Lift_Rotor (class in RCAIDE.Library.Components.Powertrain.Converters.Lift_Rotor) lift_wave_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressibility_drag) (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.lift_wave_drag) limit_input_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] linear_data() (in module RCAIDE.Library.Methods.Utilities.Chebyshev.linear_data) linear_inertial_horizontal_position() (in module RCAIDE.Library.Mission.Common.Update.linear_inertial_horizontal_position) Linear_Mach_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Linear_Mach_Constant_Rate) (class in RCAIDE.Framework.Mission.Segments.Descent.Linear_Mach_Constant_Rate)

Linear_Speed_Constant_Rate (class in RCAIDE.Framework.Mission.Segments.Climb.Linear_Speed_Constant_Rate) (class in RCAIDE.Framework.Mission.Segments.Descent.Linear_Speed_Constant_Rate) Liquid_Cooled_Wavy_Channel (class in RCAIDE.Library.Components.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel) liquid_cp_coefficients (Liquid_Hydrogen attribute) Liquid_Hydrogen (class in RCAIDE.Library.Attributes.Cryogens.Liquid_Hydrogen) (class in RCAIDE.Library.Attributes.Propellants.Liquid_Hydrogen) Liquid_Natural_Gas (class in RCAIDE.Library.Attributes.Propellants.Liquid_Natural_Gas) Liquid_Petroleum_Gas (class in RCAIDE.Library.Attributes.Propellants.Liquid_Petroleum_Gas) Lithium_Air (class in RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Air) Lithium_Ion_LFP (class in RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_LFP) Lithium_Ion_NMC (class in RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_NMC) Lithium_Sulfur (class in RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Sulfur) load() (in module RCAIDE.load) load_battery_results() (in module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_LFP) (in module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_NMC) load_kc_values() (Cross_Flow_Heat_Exchanger method) load_ke_values() (Cross_Flow_Heat_Exchanger method) LONG_UNROLL (Geodesic attribute), [1] (GeodesicCapability attribute), [1] LONGITUDE (Geodesic attribute), [1] (GeodesicCapability attribute), [1] low_pressure_compressor (Turbofan attribute) (Turbojet attribute) low_pressure_turbine (Turbofan attribute) (Turbojet attribute) (Turboshaft attribute) lower_bound (Aluminum_Air.cell.ragone attribute) (Lithium_Sulfur.cell.ragone attribute) lower_heating_value (Alcohol_Mixture attribute) (Alkane_Mixture attribute) (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Jet_A attribute) (Jet_A1 attribute) (Methane attribute) (Propane attribute) (Propanol attribute) (Propellant attribute)

M

mach_slices() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.mach_slices) Magnesium (class in RCAIDE.Library.Attributes.Materials.Magnesium) Main_Landing_Gear (class in RCAIDE.Library.Components.Landing_Gear.Main_Landing_Gear) Main_Wing (class in RCAIDE.Library.Components.Wings.Main_Wing) make_airfoil_text() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor), [1] make_beta_text_command() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) make_body_section_text() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) make_body_text() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) make_case_command() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_input_deck) make_controls_case_text() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_run_cases) make_controls_text() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) make_cs_wing_from_cs() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) make_duct_text() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_geometry) make_header_text() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor), [1] (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_geometry) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_input_deck) make_hinge_quaternion() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1] make_hub_text() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_geometry) make_link() (in module RCAIDE.Framework.Core.redirect), [1] make_pitch_rate_text_command() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) make_roll_rate_text_command() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) make_section_text() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor), [1] make_separator_text() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_geometry) make_settings_text() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_input_deck) make_span_break() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) make_span_break_from_segment() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) make_span_break_tag() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) make_span_breaks_from_cs() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) make_surface_text() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) make_trim_text_command() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) make_VLM_wings() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) make_wing_section_text() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) make_x_z_reflection() (Vertical_Tail method) (Vertical_Tail_All_Moving method) mass (Earth attribute) (Mass_Properties attribute) (Planet attribute) (Reservoir.mass_properties attribute) mass_gain_factor (Aluminum_Air attribute) (Lithium_Air.cell attribute) Mass_Properties (class in RCAIDE.Library.Components.Mass_Properties) mass_properties (Component attribute) (Network attribute) (Propellant attribute) (Wing attribute) mass_properties() (in module RCAIDE.Library.Mission.Common.Pre_Process.mass_properties) material (Reservoir attribute) Math (class in RCAIDE.Library.Methods.Geodesics.Geodesics), [1] max_area_ratio (Supersonic_Nozzle attribute) max_mass_fraction (Gaseous_Hydrogen attribute) (Jet_A attribute) (Jet_A1 attribute) (Propellant attribute) max_thickness_distribution (Rotor attribute) maximum_energy (Lithium_Ion_LFP attribute) (Lithium_Ion_NMC attribute) maximum_power (Lithium_Ion_LFP attribute) (Lithium_Ion_NMC attribute) maximum_voltage (Lithium_Ion_LFP attribute) (Lithium_Ion_NMC attribute) maxit1_ (Geodesic attribute), [1] maxit2_ (Geodesic attribute), [1] mean_radius (Earth attribute) (Planet attribute) measure() (Distance method), [1] (Geodesic_Calculate method), [1] mechanical_efficiency (Turbine attribute) melting_point (CrossLinked_Polyethylene attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) merged() (Container method) (State.Container method) Methane (class in RCAIDE.Library.Attributes.Propellants.Methane) mid_chord_alignment (Rotor attribute) min_area_ratio (Supersonic_Nozzle attribute) minimum_air_speed (Cross_Flow_Heat_Exchanger attribute) minimum_gage_thickness (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute) minimum_width (Aluminum_Alloy attribute) miscellaneous_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.miscellaneous_drag) Missions (class in RCAIDE.Framework.Mission.Missions) missions_setup() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) mixed_noise_component() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.mixed_noise_component), [1] modify_blade_geometry() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup) modify_crossflow_hex_size() (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_sizing_setup) modify_wavy_channel_HAS() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_sizing_setup) module RCAIDE.Framework RCAIDE.Framework.Analyses RCAIDE.Framework.Analyses.Aerodynamics RCAIDE.Framework.Analyses.Aerodynamics.Aerodynamics RCAIDE.Framework.Analyses.Aerodynamics.Athena_Vortex_Lattice RCAIDE.Framework.Analyses.Aerodynamics.Vortex_Lattice_Method RCAIDE.Framework.Analyses.Analysis RCAIDE.Framework.Analyses.Atmospheric RCAIDE.Framework.Analyses.Atmospheric.Atmospheric RCAIDE.Framework.Analyses.Atmospheric.Constant_Temperature RCAIDE.Framework.Analyses.Atmospheric.US_Standard_1976 RCAIDE.Framework.Analyses.Common RCAIDE.Framework.Analyses.Common.Process_Geometry RCAIDE.Framework.Analyses.Emissions RCAIDE.Framework.Analyses.Emissions.Emission_Index_Correlation_Method RCAIDE.Framework.Analyses.Emissions.Emission_Index_CRN_Method RCAIDE.Framework.Analyses.Emissions.Emissions RCAIDE.Framework.Analyses.Energy RCAIDE.Framework.Analyses.Energy.Energy RCAIDE.Framework.Analyses.Geodesics RCAIDE.Framework.Analyses.Geodesics.Geodesics RCAIDE.Framework.Analyses.Noise RCAIDE.Framework.Analyses.Noise.Correlation_Buildup RCAIDE.Framework.Analyses.Noise.Frequency_Domain_Buildup RCAIDE.Framework.Analyses.Noise.Noise RCAIDE.Framework.Analyses.Planets RCAIDE.Framework.Analyses.Planets.Earth RCAIDE.Framework.Analyses.Planets.Planet RCAIDE.Framework.Analyses.Process RCAIDE.Framework.Analyses.Propulsion RCAIDE.Framework.Analyses.Propulsion.Ducted_Fan_Design_Code RCAIDE.Framework.Analyses.Settings RCAIDE.Framework.Analyses.Stability RCAIDE.Framework.Analyses.Stability.Athena_Vortex_Lattice RCAIDE.Framework.Analyses.Stability.Stability RCAIDE.Framework.Analyses.Stability.Vortex_Lattice_Method RCAIDE.Framework.Analyses.Vehicle RCAIDE.Framework.Analyses.Weights RCAIDE.Framework.Analyses.Weights.Conventional RCAIDE.Framework.Analyses.Weights.Electric RCAIDE.Framework.Analyses.Weights.Hybrid RCAIDE.Framework.Analyses.Weights.Hydrogen RCAIDE.Framework.Analyses.Weights.Weights RCAIDE.Framework.Core RCAIDE.Framework.Core.Arrays RCAIDE.Framework.Core.Container RCAIDE.Framework.Core.ContainerOrdered RCAIDE.Framework.Core.Data RCAIDE.Framework.Core.DataOrdered RCAIDE.Framework.Core.Diffed_Data RCAIDE.Framework.Core.redirect RCAIDE.Framework.Core.Units RCAIDE.Framework.Core.Utilities RCAIDE.Framework.External_Interfaces RCAIDE.Framework.External_Interfaces.OpenVSP RCAIDE.Framework.External_Interfaces.OpenVSP.export_vsp_vehicle RCAIDE.Framework.External_Interfaces.OpenVSP.get_fuel_tank_properties RCAIDE.Framework.External_Interfaces.OpenVSP.get_vsp_measurements RCAIDE.Framework.External_Interfaces.OpenVSP.import_vsp_vehicle RCAIDE.Framework.External_Interfaces.OpenVSP.mach_slices RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_nacelle RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing RCAIDE.Framework.External_Interfaces.OpenVSP.write_vsp_mesh RCAIDE.Framework.Mission RCAIDE.Framework.Mission.Common RCAIDE.Framework.Mission.Common.Conditions RCAIDE.Framework.Mission.Common.Numerics RCAIDE.Framework.Mission.Common.Residuals RCAIDE.Framework.Mission.Common.Results RCAIDE.Framework.Mission.Common.State RCAIDE.Framework.Mission.Common.Unknowns RCAIDE.Framework.Mission.Missions RCAIDE.Framework.Mission.Segments RCAIDE.Framework.Mission.Segments.Climb RCAIDE.Framework.Mission.Segments.Climb.Constant_CAS_Constant_Rate RCAIDE.Framework.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle RCAIDE.Framework.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate RCAIDE.Framework.Mission.Segments.Climb.Constant_EAS_Constant_Rate RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Constant_Angle RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Constant_Rate RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Linear_Altitude RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Constant_Angle RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Constant_Rate RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Linear_Altitude RCAIDE.Framework.Mission.Segments.Climb.Constant_Throttle_Constant_Speed RCAIDE.Framework.Mission.Segments.Climb.Linear_Mach_Constant_Rate RCAIDE.Framework.Mission.Segments.Climb.Linear_Speed_Constant_Rate RCAIDE.Framework.Mission.Segments.Cruise RCAIDE.Framework.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude RCAIDE.Framework.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude RCAIDE.Framework.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter RCAIDE.Framework.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude RCAIDE.Framework.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter RCAIDE.Framework.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude RCAIDE.Framework.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude RCAIDE.Framework.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter RCAIDE.Framework.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude RCAIDE.Framework.Mission.Segments.Cruise.Curved_Constant_Radius_Constant_Speed_Constant_Altitude RCAIDE.Framework.Mission.Segments.Descent RCAIDE.Framework.Mission.Segments.Descent.Constant_CAS_Constant_Rate RCAIDE.Framework.Mission.Segments.Descent.Constant_EAS_Constant_Rate RCAIDE.Framework.Mission.Segments.Descent.Constant_Speed_Constant_Angle RCAIDE.Framework.Mission.Segments.Descent.Constant_Speed_Constant_Rate RCAIDE.Framework.Mission.Segments.Descent.Linear_Mach_Constant_Rate RCAIDE.Framework.Mission.Segments.Descent.Linear_Speed_Constant_Rate RCAIDE.Framework.Mission.Segments.Evaluate RCAIDE.Framework.Mission.Segments.Ground RCAIDE.Framework.Mission.Segments.Ground.Battery_Discharge RCAIDE.Framework.Mission.Segments.Ground.Battery_Recharge RCAIDE.Framework.Mission.Segments.Ground.Ground RCAIDE.Framework.Mission.Segments.Ground.Landing RCAIDE.Framework.Mission.Segments.Ground.Takeoff RCAIDE.Framework.Mission.Segments.Segment RCAIDE.Framework.Mission.Segments.Single_Point RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_AVL_Trimmed RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion 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RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.append_turbojet_conditions RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_thurst RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_turbojet_performance RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.design_turbojet RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.size_core RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.append_turboprop_conditions RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_thrust RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_turboprop_performance RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.design_turboprop RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.size_core RCAIDE.Library.Methods.Powertrain.setup_operating_conditions RCAIDE.Library.Methods.Powertrain.Sources RCAIDE.Library.Methods.Powertrain.Sources.Batteries RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Aluminum_Air RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Aluminum_Air.compute_al_air_cell_performance RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.append_battery_conditions RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.compute_module_properties RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_mass_gain_rate RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_ragone_properties RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_specific_power RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_total_mass_gain RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.size_module_from_energy_and_power RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.size_module_from_mass RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.compute_lfp_cell_performance RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.update_lfp_cell_age RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.compute_nmc_cell_performance RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.update_nmc_cell_age RCAIDE.Library.Methods.Powertrain.Sources.Cryogenic_Tanks RCAIDE.Library.Methods.Powertrain.Sources.Cryogenic_Tanks.append_cryogenic_tank_conditions RCAIDE.Library.Methods.Powertrain.Sources.Fuel_Tanks RCAIDE.Library.Methods.Powertrain.Sources.Fuel_Tanks.append_fuel_tank_conditions RCAIDE.Library.Methods.Powertrain.Systems RCAIDE.Library.Methods.Powertrain.Systems.append_avionics_conditions RCAIDE.Library.Methods.Powertrain.Systems.append_payload_conditions RCAIDE.Library.Methods.Powertrain.Systems.compute_avionics_power_draw RCAIDE.Library.Methods.Powertrain.Systems.compute_payload_power_draw RCAIDE.Library.Methods.skip RCAIDE.Library.Methods.Stability RCAIDE.Library.Methods.Stability.compute_dynamic_flight_modes RCAIDE.Library.Methods.Thermal_Management RCAIDE.Library.Methods.Thermal_Management.Batteries RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.air_cooled_performance RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.append_air_cooled_conditions RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.append_wavy_channel_conditions RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.design_wavy_channel RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_geometry_setup RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_rating_model RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_sizing_setup RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.append_cross_flow_heat_exchanger_conditions RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.compute_heat_exhanger_factors RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_geometry_setup RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_sizing_setup RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_hex_rating_model RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.design_cross_flow_heat_exchanger RCAIDE.Library.Methods.Thermal_Management.Reservoirs RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.append_reservoir_conditions RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.compute_mixing_temperature RCAIDE.Library.Methods.Utilities RCAIDE.Library.Methods.Utilities.Chebyshev RCAIDE.Library.Methods.Utilities.Chebyshev.chebyshev_data RCAIDE.Library.Methods.Utilities.Chebyshev.linear_data RCAIDE.Library.Methods.Utilities.Cubic_Spline_Blender RCAIDE.Library.Methods.Utilities.latin_hypercube_sampling RCAIDE.Library.Mission RCAIDE.Library.Mission.Common RCAIDE.Library.Mission.Common.Initialize RCAIDE.Library.Mission.Common.Initialize.differentials_altitude RCAIDE.Library.Mission.Common.Initialize.differentials_dimensionless RCAIDE.Library.Mission.Common.Initialize.energy RCAIDE.Library.Mission.Common.Initialize.inertial_position RCAIDE.Library.Mission.Common.Initialize.planet_position RCAIDE.Library.Mission.Common.Initialize.time RCAIDE.Library.Mission.Common.Initialize.weights RCAIDE.Library.Mission.Common.Pre_Process RCAIDE.Library.Mission.Common.Pre_Process.aerodynamics RCAIDE.Library.Mission.Common.Pre_Process.emissions RCAIDE.Library.Mission.Common.Pre_Process.energy RCAIDE.Library.Mission.Common.Pre_Process.mass_properties RCAIDE.Library.Mission.Common.Pre_Process.set_residuals_and_unknowns RCAIDE.Library.Mission.Common.Pre_Process.stability RCAIDE.Library.Mission.Common.Residuals RCAIDE.Library.Mission.Common.Residuals.flight_dynamics RCAIDE.Library.Mission.Common.Segments RCAIDE.Library.Mission.Common.Unpack_Unknowns RCAIDE.Library.Mission.Common.Unpack_Unknowns.control_surfaces RCAIDE.Library.Mission.Common.Unpack_Unknowns.energy RCAIDE.Library.Mission.Common.Unpack_Unknowns.ground RCAIDE.Library.Mission.Common.Unpack_Unknowns.orientation RCAIDE.Library.Mission.Common.Update RCAIDE.Library.Mission.Common.Update.acceleration RCAIDE.Library.Mission.Common.Update.aerodynamics RCAIDE.Library.Mission.Common.Update.altitude RCAIDE.Library.Mission.Common.Update.angular_acceleration RCAIDE.Library.Mission.Common.Update.atmosphere RCAIDE.Library.Mission.Common.Update.curvilinear_inertial_horizontal_position RCAIDE.Library.Mission.Common.Update.differentials_time RCAIDE.Library.Mission.Common.Update.emissions RCAIDE.Library.Mission.Common.Update.energy RCAIDE.Library.Mission.Common.Update.forces RCAIDE.Library.Mission.Common.Update.freestream RCAIDE.Library.Mission.Common.Update.gravity RCAIDE.Library.Mission.Common.Update.ground_forces RCAIDE.Library.Mission.Common.Update.kinematics RCAIDE.Library.Mission.Common.Update.linear_inertial_horizontal_position RCAIDE.Library.Mission.Common.Update.moments RCAIDE.Library.Mission.Common.Update.noise RCAIDE.Library.Mission.Common.Update.orientations RCAIDE.Library.Mission.Common.Update.planet_position RCAIDE.Library.Mission.Common.Update.stability RCAIDE.Library.Mission.Common.Update.thrust RCAIDE.Library.Mission.Common.Update.weights RCAIDE.Library.Mission.Segments RCAIDE.Library.Mission.Segments.Climb RCAIDE.Library.Mission.Segments.Climb.Constant_CAS_Constant_Rate RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate RCAIDE.Library.Mission.Segments.Climb.Constant_EAS_Constant_Rate RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Angle RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Rate RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Linear_Altitude RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Rate RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Linear_Altitude RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed RCAIDE.Library.Mission.Segments.Climb.Linear_Mach_Constant_Rate RCAIDE.Library.Mission.Segments.Climb.Linear_Speed_Constant_Rate RCAIDE.Library.Mission.Segments.Cruise RCAIDE.Library.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude RCAIDE.Library.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude RCAIDE.Library.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter RCAIDE.Library.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude RCAIDE.Library.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter RCAIDE.Library.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude RCAIDE.Library.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude RCAIDE.Library.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude RCAIDE.Library.Mission.Segments.Cruise.Curved_Constant_Radius_Constant_Speed_Constant_Altitude RCAIDE.Library.Mission.Segments.Descent RCAIDE.Library.Mission.Segments.Descent.Constant_CAS_Constant_Rate RCAIDE.Library.Mission.Segments.Descent.Constant_EAS_Constant_Rate RCAIDE.Library.Mission.Segments.Descent.Constant_Speed_Constant_Angle RCAIDE.Library.Mission.Segments.Descent.Constant_Speed_Constant_Rate RCAIDE.Library.Mission.Segments.Descent.Linear_Mach_Constant_Rate RCAIDE.Library.Mission.Segments.Descent.Linear_Speed_Constant_Rate RCAIDE.Library.Mission.Segments.Ground RCAIDE.Library.Mission.Segments.Ground.Battery_Charge_Discharge RCAIDE.Library.Mission.Segments.Ground.Landing RCAIDE.Library.Mission.Segments.Ground.Takeoff RCAIDE.Library.Mission.Segments.Single_Point RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_AVL_Trimmed RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Throttle RCAIDE.Library.Mission.Segments.Transition RCAIDE.Library.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb RCAIDE.Library.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude RCAIDE.Library.Mission.Segments.Untrimmed RCAIDE.Library.Mission.Segments.Untrimmed.Untrimmed RCAIDE.Library.Mission.Segments.Vertical_Flight RCAIDE.Library.Mission.Segments.Vertical_Flight.Climb RCAIDE.Library.Mission.Segments.Vertical_Flight.Descent RCAIDE.Library.Mission.Segments.Vertical_Flight.Hover RCAIDE.Library.Mission.Solver RCAIDE.Library.Mission.Solver.converge RCAIDE.Library.Mission.Solver.expand_state RCAIDE.Library.Plots RCAIDE.Library.Plots.Aerodynamics RCAIDE.Library.Plots.Aerodynamics.plot_aerodynamic_coefficients RCAIDE.Library.Plots.Aerodynamics.plot_aerodynamic_forces RCAIDE.Library.Plots.Aerodynamics.plot_aircraft_aerodynamics RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_boundary_layer_properties RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_polar_files RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_polars RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_surface_forces RCAIDE.Library.Plots.Aerodynamics.plot_disc_and_power_loading RCAIDE.Library.Plots.Aerodynamics.plot_drag_components RCAIDE.Library.Plots.Aerodynamics.plot_lift_distribution RCAIDE.Library.Plots.Aerodynamics.plot_rotor_conditions RCAIDE.Library.Plots.Aerodynamics.plot_rotor_disc_performance RCAIDE.Library.Plots.Aerodynamics.plot_rotor_performance RCAIDE.Library.Plots.Aerodynamics.plot_surface_pressures RCAIDE.Library.Plots.Common RCAIDE.Library.Plots.Emissions RCAIDE.Library.Plots.Emissions.plot_CO2e_emissions RCAIDE.Library.Plots.Energy RCAIDE.Library.Plots.Energy.plot_altitude_sfc_weight RCAIDE.Library.Plots.Energy.plot_battery_cell_conditions RCAIDE.Library.Plots.Energy.plot_battery_degradation RCAIDE.Library.Plots.Energy.plot_battery_module_C_rates RCAIDE.Library.Plots.Energy.plot_battery_module_conditions RCAIDE.Library.Plots.Energy.plot_battery_pack_conditions RCAIDE.Library.Plots.Energy.plot_battery_ragone_diagram RCAIDE.Library.Plots.Energy.plot_battery_temperature RCAIDE.Library.Plots.Energy.plot_crogenic_fuel_consumption RCAIDE.Library.Plots.Energy.plot_electric_propulsor_efficiencies RCAIDE.Library.Plots.Energy.plot_fuel_consumption RCAIDE.Library.Plots.Energy.plot_propulsor_throttles RCAIDE.Library.Plots.Geometry RCAIDE.Library.Plots.Geometry.Common RCAIDE.Library.Plots.Geometry.Common.contour_surface_slice RCAIDE.Library.Plots.Geometry.plot_3d_fuselage RCAIDE.Library.Plots.Geometry.plot_3d_nacelle RCAIDE.Library.Plots.Geometry.plot_3d_rotor RCAIDE.Library.Plots.Geometry.plot_3d_vehicle RCAIDE.Library.Plots.Geometry.plot_3d_vehicle_vlm_panelization RCAIDE.Library.Plots.Geometry.plot_3d_wing RCAIDE.Library.Plots.Geometry.plot_airfoil RCAIDE.Library.Plots.Geometry.plot_layout_of_passenger_accommodations RCAIDE.Library.Plots.Geometry.plot_rotor RCAIDE.Library.Plots.Mission RCAIDE.Library.Plots.Mission.plot_aircraft_velocities RCAIDE.Library.Plots.Mission.plot_flight_conditions RCAIDE.Library.Plots.Mission.plot_flight_trajectory RCAIDE.Library.Plots.Noise RCAIDE.Library.Plots.Noise.plot_2D_noise_contour RCAIDE.Library.Plots.Noise.plot_3D_noise_contour RCAIDE.Library.Plots.Noise.plot_noise_level RCAIDE.Library.Plots.Noise.post_process_noise_data RCAIDE.Library.Plots.Stability RCAIDE.Library.Plots.Stability.plot_flight_forces_and_moments RCAIDE.Library.Plots.Stability.plot_lateral_stability RCAIDE.Library.Plots.Stability.plot_longitudinal_stability RCAIDE.Library.Plots.Thermal_Management RCAIDE.Library.Plots.Thermal_Management.plot_air_cooled_conditions RCAIDE.Library.Plots.Thermal_Management.plot_cross_flow_heat_exchanger_conditions RCAIDE.Library.Plots.Thermal_Management.plot_reservoir_conditions RCAIDE.Library.Plots.Thermal_Management.plot_thermal_management_performance RCAIDE.Library.Plots.Thermal_Management.plot_wavy_channel_conditions RCAIDE.Library.Plots.Topography RCAIDE.Library.Plots.Topography.plot_elevation_contours RCAIDE.Library.Plots.Weights RCAIDE.Library.Plots.Weights.plot_weight_breakdown RCAIDE.load RCAIDE.save RCAIDE.Vehicle

modulus_of_elasticity (CrossLinked_Polyethylene attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) molecular_mass (Air attribute) (CO2 attribute) (Gas attribute) (Gaseous_Hydrogen attribute) (Steam attribute) molecular_weight (Rocket_LH2 attribute) (Rocket_RP1 attribute) moment_of_inertia() (All_Moving_Surface method) (Horizontal_Tail method) (Main_Wing method) (Stabilator method) (Vertical_Tail method) (Vertical_Tail_All_Moving method) moments() (in module RCAIDE.Library.Mission.Common.Update.moments) moments_of_inertia (Mass_Properties attribute) motor (Electric_Ducted_Fan attribute) (Electric_Rotor attribute) motor_stack_length (PMSM_Motor attribute) mu_0 (PMSM_Motor attribute) mu_r (PMSM_Motor attribute) MW_C (Reformer attribute) MW_F (Reformer attribute) MW_H2 (Reformer attribute) MW_S (Reformer attribute)

N

N_comb (Combustor attribute) N_PZ (Combustor attribute) N_SZ (Combustor attribute) nA1_ (Geodesic attribute), [1] nA2_ (Geodesic attribute), [1] nA3_ (Geodesic attribute), [1] nA3x_ (Geodesic attribute), [1] nac_vel_to_body() (Nacelle method) NACA_4_Series_Airfoil (class in RCAIDE.Library.Components.Airfoils.NACA_4_Series_Airfoil) NACA_4_Series_code (NACA_4_Series_Airfoil attribute) Nacelle (class in RCAIDE.Library.Components.Nacelles.Nacelle) nacelle (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) nacelle_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_nacelle) nC1_ (Geodesic attribute), [1] nC1p_ (Geodesic attribute), [1] nC2_ (Geodesic attribute), [1] nC3_ (Geodesic attribute), [1] nC3x_ (Geodesic attribute), [1] nC4_ (Geodesic attribute), [1] nC4x_ (Geodesic attribute), [1] Network (class in RCAIDE.Framework.Networks.Network) (class in RCAIDE.Library.Components.Network) Network.Container (class in RCAIDE.Framework.Networks.Network) (class in RCAIDE.Library.Components.Network) new_tensor() (in module RCAIDE.Framework.Core.Utilities), [1] next (Airfoil attribute) (Circle_Segment attribute) (Ellipse_Segment attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute)

Nexus (class in RCAIDE.Framework.Optimization.Common.Nexus) Nickel (class in RCAIDE.Library.Attributes.Materials.Nickel) no_load_current (DC_Generator attribute) (DC_Motor attribute) (PMSM_Generator attribute) no_surrogate() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.build_VLM_surrogates) Noise (class in RCAIDE.Framework.Analyses.Noise.Noise) noise() (in module RCAIDE.Library.Mission.Common.Update.noise) noise_directivities() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.noise_directivities) noise_source_location() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.noise_source_location), [1] nominal_capacity (Electrical_Bus attribute) nonuniform_freestream (Rotor attribute) norm() (Math static method), [1] nose_curvature (Fuselage attribute) Nose_Landing_Gear (class in RCAIDE.Library.Components.Landing_Gear.Nose_Landing_Gear) number_azimuthal_stations (Rotor attribute) number_of_assigned_PSR_1st_mixers (Combustor attribute) number_of_assigned_PSR_2nd_mixers (Combustor attribute) number_of_blades (Rotor attribute) number_of_cells (Lithium_Ion_LFP attribute) number_of_combustors (Combustor attribute) number_of_points (Airfoil attribute) number_of_radial_stations (Ducted_Fan attribute) number_of_rotor_blades (Ducted_Fan attribute) number_of_turns (PMSM_Motor attribute) Numerics (class in RCAIDE.Framework.Mission.Common.Numerics)

O

objective() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator) (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor) (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_propeller) (Nexus method) objgetattrib() (in module RCAIDE.Framework.Core.Data) oei (Lift_Rotor attribute) (Prop_Rotor attribute) ones_row() (Conditions method) ones_row_m1() (Conditions method) ones_row_m2() (Conditions method) OpenVSP_flow_through (Turbofan attribute) (Turbojet attribute) optimization_parameters (Prop_Rotor attribute) optimization_setup() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.optimization_setup) optimize() (Trust_Region_Optimization method), [1] orientation() (in module RCAIDE.Library.Mission.Common.Unpack_Unknowns.orientation) orientation_euler_angles (Ducted_Fan attribute) (Generic_Battery_Module attribute) (Lift_Rotor attribute) (Nacelle attribute) (Prop_Rotor attribute) (Propeller attribute) (Rotor attribute) (Segment attribute)

orientation_product() (in module RCAIDE.Framework.Core.Utilities), [1] orientation_transpose() (in module RCAIDE.Framework.Core.Utilities), [1] orientations() (in module RCAIDE.Library.Mission.Common.Update.orientations) origin (Boom attribute) (Component attribute) (Fuselage attribute) (Nacelle attribute) (Network attribute) (System attribute) (Wing attribute) OUT_ALL (Geodesic attribute), [1] (GeodesicCapability attribute), [1] OUT_MASK (Geodesic attribute), [1] (GeodesicCapability attribute), [1] output (class in RCAIDE.Framework.Core.redirect), [1] outputs (Network attribute)

P

pack_array() (Data method) pack_electric_ducted_fan_residuals() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.pack_electric_ducted_fan_residuals) pack_electric_rotor_residuals() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.pack_electric_rotor_residuals) pack_internal_combustion_engine_residuals() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.pack_internal_combustion_engine_residuals) pack_propulsor_residuals() (Constant_Speed_Internal_Combustion_Engine method) (Electric_Ducted_Fan method) (Electric_Rotor method) (Internal_Combustion_Engine method) (Turbofan method) (Turbojet method) (Turboprop method) (Turboshaft method) Paint (class in RCAIDE.Library.Attributes.Materials.Paint) panel_geometry() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.panel_geometry) parasite_drag_fuselage() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_fuselage) parasite_drag_nacelle() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_nacelle) parasite_drag_pylon() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_pylon) parasite_drag_wing() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_wing) parasite_total() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_total) particle_swarm_optimization() (in module RCAIDE.Framework.Optimization.Packages.particle_swarm.particle_swarm_optimization) Payload (class in RCAIDE.Library.Components.Payloads.Payload) payload (Electrical_Bus attribute) percent_glycol (Glycol_Water attribute) percent_span_location (Segment attribute) percent_x_location (Circle_Segment attribute) (Ellipse_Segment attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute) percent_y_location (Circle_Segment attribute) (Ellipse_Segment attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute) percent_z_location (Circle_Segment attribute) (Ellipse_Segment attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute) Perfluoroalkoxy (class in RCAIDE.Library.Attributes.Materials.Perfluoroalkoxy) phase_offset_angle (Rotor attribute) phi_SZ (Combustor attribute) Planet (class in RCAIDE.Framework.Analyses.Planets.Planet) (class in RCAIDE.Library.Attributes.Planets.Planet) planet (Constant_Temperature attribute) (US_Standard_1976 attribute) planet_position() (in module RCAIDE.Library.Mission.Common.Initialize.planet_position) (in module RCAIDE.Library.Mission.Common.Update.planet_position) plot_2D_noise_contour() (in module RCAIDE.Library.Plots.Noise.plot_2D_noise_contour) plot_3d_energy_network() (in module RCAIDE.Library.Plots.Geometry.plot_3d_vehicle) plot_3d_fuselage() (in module RCAIDE.Library.Plots.Geometry.plot_3d_fuselage), [1] plot_3d_nacelle() (in module RCAIDE.Library.Plots.Geometry.plot_3d_nacelle) plot_3D_noise_contour() (in module RCAIDE.Library.Plots.Noise.plot_3D_noise_contour) plot_3d_rotor() (in module RCAIDE.Library.Plots.Geometry.plot_3d_rotor) plot_3d_vehicle() (in module RCAIDE.Library.Plots.Geometry.plot_3d_vehicle) plot_3d_vehicle_vlm_panelization() (in module RCAIDE.Library.Plots.Geometry.plot_3d_vehicle_vlm_panelization) plot_3d_wing() (in module RCAIDE.Library.Plots.Geometry.plot_3d_wing) plot_aerodynamic_coefficients() (in module RCAIDE.Library.Plots.Aerodynamics.plot_aerodynamic_coefficients) plot_aerodynamic_forces() (in module RCAIDE.Library.Plots.Aerodynamics.plot_aerodynamic_forces) plot_air_cooled_conditions() (in module RCAIDE.Library.Plots.Thermal_Management.plot_air_cooled_conditions) plot_aircraft_aerodynamics() (in module RCAIDE.Library.Plots.Aerodynamics.plot_aircraft_aerodynamics) plot_aircraft_velocities() (in module RCAIDE.Library.Plots.Mission.plot_aircraft_velocities) plot_airfoil() (in module RCAIDE.Library.Plots.Geometry.plot_airfoil) plot_airfoil_boundary_layer_properties() (in module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_boundary_layer_properties) plot_airfoil_polar_files() (in module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_polar_files) plot_airfoil_polars() (in module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_polars) plot_airfoil_surface_forces() (in module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_surface_forces) plot_altitude_sfc_weight() (in module RCAIDE.Library.Plots.Energy.plot_altitude_sfc_weight) plot_battery_cell_conditions() (in module RCAIDE.Library.Plots.Energy.plot_battery_cell_conditions) plot_battery_degradation() (in module RCAIDE.Library.Plots.Energy.plot_battery_degradation) plot_battery_module_C_rates() (in module RCAIDE.Library.Plots.Energy.plot_battery_module_C_rates) plot_battery_module_conditions() (in module RCAIDE.Library.Plots.Energy.plot_battery_module_conditions) plot_battery_pack_conditions() (in module RCAIDE.Library.Plots.Energy.plot_battery_pack_conditions) plot_battery_ragone_diagram() (in module RCAIDE.Library.Plots.Energy.plot_battery_ragone_diagram) plot_battery_temperature() (in module RCAIDE.Library.Plots.Energy.plot_battery_temperature) plot_CO2e_emissions() (in module RCAIDE.Library.Plots.Emissions.plot_CO2e_emissions) plot_cross_flow_heat_exchanger_conditions() (in module RCAIDE.Library.Plots.Thermal_Management.plot_cross_flow_heat_exchanger_conditions) plot_disc_and_power_loading() (in module RCAIDE.Library.Plots.Aerodynamics.plot_disc_and_power_loading) plot_drag_components() (in module RCAIDE.Library.Plots.Aerodynamics.plot_drag_components) plot_electric_propulsor_efficiencies() (in module RCAIDE.Library.Plots.Energy.plot_electric_propulsor_efficiencies) plot_elevation_contours() (in module RCAIDE.Library.Plots.Topography.plot_elevation_contours) plot_flight_conditions() (in module RCAIDE.Library.Plots.Mission.plot_flight_conditions) plot_flight_forces_and_moments() (in module RCAIDE.Library.Plots.Stability.plot_flight_forces_and_moments) plot_flight_trajectory() (in module RCAIDE.Library.Plots.Mission.plot_flight_trajectory) plot_fuel_consumption() (in module RCAIDE.Library.Plots.Energy.plot_crogenic_fuel_consumption), [1] (in module RCAIDE.Library.Plots.Energy.plot_fuel_consumption) plot_lateral_stability() (in module RCAIDE.Library.Plots.Stability.plot_lateral_stability) plot_layout_of_passenger_accommodations() (in module RCAIDE.Library.Plots.Geometry.plot_layout_of_passenger_accommodations) plot_lift_distribution() (in module RCAIDE.Library.Plots.Aerodynamics.plot_lift_distribution) plot_longitudinal_stability() (in module RCAIDE.Library.Plots.Stability.plot_longitudinal_stability) plot_noise_level() (in module RCAIDE.Library.Plots.Noise.plot_noise_level) plot_operating_conditions() (Air_Cooled method) (Cross_Flow_Heat_Exchanger method) (Liquid_Cooled_Wavy_Channel method) (Reservoir method) plot_propulsor_data() (in module RCAIDE.Library.Plots.Aerodynamics.plot_disc_and_power_loading) (in module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_conditions) plot_propulsor_throttles() (in module RCAIDE.Library.Plots.Energy.plot_propulsor_throttles) plot_quantity() (in module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_boundary_layer_properties) plot_reservoir_conditions() (in module RCAIDE.Library.Plots.Thermal_Management.plot_reservoir_conditions)

plot_rotor() (in module RCAIDE.Library.Plots.Geometry.plot_rotor) plot_rotor_conditions() (in module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_conditions) plot_rotor_disc_performance() (in module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_disc_performance) plot_rotor_performance() (in module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_performance) plot_surface_pressures() (in module RCAIDE.Library.Plots.Aerodynamics.plot_surface_pressures) plot_thermal_management_performance() (in module RCAIDE.Library.Plots.Thermal_Management.plot_thermal_management_performance) plot_wavy_channel_conditions() (in module RCAIDE.Library.Plots.Thermal_Management.plot_wavy_channel_conditions) plot_weight_breakdown() (in module RCAIDE.Library.Plots.Weights.plot_weight_breakdown) plug_diameter (Turbofan attribute) PMSM_Generator (class in RCAIDE.Library.Components.Powertrain.Converters.PMSM_Generator) PMSM_Motor (class in RCAIDE.Library.Components.Powertrain.Converters.PMSM_Motor) PNL_noise_metric() (in module RCAIDE.Library.Methods.Noise.Metrics.PNL_noise_metric) polar_files (Airfoil attribute) polars (Airfoil attribute) Polyetherimide (class in RCAIDE.Library.Attributes.Materials.Polyetherimide) Polyimide (class in RCAIDE.Library.Attributes.Materials.Polyimide) Polytetrafluoroethylene (class in RCAIDE.Library.Attributes.Materials.Polytetrafluoroethylene) polytropic_efficiency (Compression_Nozzle attribute) (Compressor attribute) (Expansion_Nozzle attribute) (Fan attribute) (Supersonic_Nozzle attribute) (Turbine attribute) polyval() (Math static method), [1] populate_body_sections() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures), [1] populate_control_sections() (in module RCAIDE.Library.Methods.Geometry.Planform.populate_control_sections) populate_wing_sections() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures), [1] post_process() (Aerodynamics method) (Analysis method) (Analysis.Container method) (Container method) (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup) (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_sizing_setup) (in module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_sizing_setup) (Segment method) post_process_certification_noise_data() (in module RCAIDE.Library.Methods.Performance.compute_noise_certification_data), [1] post_process_noise_data() (in module RCAIDE.Library.Plots.Noise.post_process_noise_data) post_processing() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) post_stall_coefficients() (in module RCAIDE.Library.Methods.Aerodynamics.AERODAS.post_stall_coefficients) postprocess_VD() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_VD_helpers), [1] power() (Avionics method) power_draw (Avionics attribute) (Payload attribute) power_specific_fuel_consumption (Engine attribute) power_split_ratio (DC_Generator attribute) (DC_Motor attribute) (Electrical_Bus attribute) (Engine attribute) (Lithium_Ion_LFP attribute) (PMSM_Generator attribute) Prandtl_number (Glycol_Water attribute) (PMSM_Motor attribute) pre_stall_coefficients() (in module RCAIDE.Library.Methods.Aerodynamics.AERODAS.pre_stall_coefficients) pressure (Gaseous_Hydrogen attribute) pressure_ratio (Compression_Nozzle attribute) (Compressor attribute) (Expansion_Nozzle attribute) (Fan attribute) (Supersonic_Nozzle attribute) pressure_ratio_to_SPL_arithmetic() (in module RCAIDE.Library.Methods.Noise.Common.decibel_arithmetic), [1] pressure_recovery (Compression_Nozzle attribute) (Supersonic_Nozzle attribute) prev (Airfoil attribute) (Circle_Segment attribute) (Ellipse_Segment attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute) primary_noise_component() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.primary_noise_component), [1] procedure_setup() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup) Process (class in RCAIDE.Framework.Analyses.Process) process (Emission_Index_Correlation_Method attribute) Process_Geometry (class in RCAIDE.Framework.Analyses.Common.Process_Geometry) profile_drag_coefficient (Rotor attribute) Prop_Rotor (class in RCAIDE.Library.Components.Powertrain.Converters.Prop_Rotor) prop_vel_to_body() (Rotor method) Propane (class in RCAIDE.Library.Attributes.Propellants.Propane) Propanol (class in RCAIDE.Library.Attributes.Propellants.Propanol) Propellant (class in RCAIDE.Library.Attributes.Propellants.Propellant) propellant_1 (Alcohol_Mixture attribute) (Alkane_Mixture attribute) propellant_1_mass_fraction (Alcohol_Mixture attribute) (Alkane_Mixture attribute) propellant_2 (Alcohol_Mixture attribute) (Alkane_Mixture attribute) propellant_2_mass_fraction (Alcohol_Mixture attribute) (Alkane_Mixture attribute) Propeller (class in RCAIDE.Library.Components.Powertrain.Converters.Propeller) propeller (Constant_Speed_Internal_Combustion_Engine attribute) (Internal_Combustion_Engine attribute) propeller_aerodynamic_analysis() (in module RCAIDE.Library.Methods.Performance.propeller_aerodynamic_analysis), [1] propeller_efficiency (Turboprop attribute) Property (class in RCAIDE.Framework.Core.DataOrdered) Propulsor (class in RCAIDE.Library.Components.Powertrain.Propulsors.Propulsor) Proton_Exchange_Membrane_Fuel_Cell (class in RCAIDE.Library.Components.Powertrain.Converters.Proton_Exchange_Membrane_Fuel_Cell) Pump (class in RCAIDE.Library.Components.Thermal_Management.Accessories.Pump) purge_files() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.purge_files) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.purge_files) PyOpt_Problem() (in module RCAIDE.Framework.Optimization.Packages.pyopt.pyopt_setup), [1] Pyopt_Solve() (in module RCAIDE.Framework.Optimization.Packages.pyopt.pyopt_setup), [1]

R

radius (Circle_Segment attribute) (Rounded_Rectangle_Segment attribute) (Super_Ellipse_Segment attribute) radius_distribution (Rotor attribute) Ram (class in RCAIDE.Library.Components.Powertrain.Converters.Ram) ram (Turbofan attribute) (Turbojet attribute) (Turboshaft attribute) rated_speed (Engine attribute) RCAIDE.Framework module RCAIDE.Framework.Analyses module RCAIDE.Framework.Analyses.Aerodynamics module RCAIDE.Framework.Analyses.Aerodynamics.Aerodynamics module RCAIDE.Framework.Analyses.Aerodynamics.Athena_Vortex_Lattice module RCAIDE.Framework.Analyses.Aerodynamics.Vortex_Lattice_Method module RCAIDE.Framework.Analyses.Analysis module RCAIDE.Framework.Analyses.Atmospheric module RCAIDE.Framework.Analyses.Atmospheric.Atmospheric module RCAIDE.Framework.Analyses.Atmospheric.Constant_Temperature module RCAIDE.Framework.Analyses.Atmospheric.US_Standard_1976 module RCAIDE.Framework.Analyses.Common module RCAIDE.Framework.Analyses.Common.Process_Geometry module RCAIDE.Framework.Analyses.Emissions module RCAIDE.Framework.Analyses.Emissions.Emission_Index_Correlation_Method module RCAIDE.Framework.Analyses.Emissions.Emission_Index_CRN_Method module RCAIDE.Framework.Analyses.Emissions.Emissions module RCAIDE.Framework.Analyses.Energy module RCAIDE.Framework.Analyses.Energy.Energy module RCAIDE.Framework.Analyses.Geodesics module RCAIDE.Framework.Analyses.Geodesics.Geodesics module RCAIDE.Framework.Analyses.Noise module RCAIDE.Framework.Analyses.Noise.Correlation_Buildup module RCAIDE.Framework.Analyses.Noise.Frequency_Domain_Buildup module RCAIDE.Framework.Analyses.Noise.Noise module RCAIDE.Framework.Analyses.Planets module RCAIDE.Framework.Analyses.Planets.Earth module RCAIDE.Framework.Analyses.Planets.Planet module RCAIDE.Framework.Analyses.Process module RCAIDE.Framework.Analyses.Propulsion module RCAIDE.Framework.Analyses.Propulsion.Ducted_Fan_Design_Code module RCAIDE.Framework.Analyses.Settings module RCAIDE.Framework.Analyses.Stability module RCAIDE.Framework.Analyses.Stability.Athena_Vortex_Lattice module RCAIDE.Framework.Analyses.Stability.Stability module RCAIDE.Framework.Analyses.Stability.Vortex_Lattice_Method module RCAIDE.Framework.Analyses.Vehicle module RCAIDE.Framework.Analyses.Weights module RCAIDE.Framework.Analyses.Weights.Conventional module RCAIDE.Framework.Analyses.Weights.Electric module RCAIDE.Framework.Analyses.Weights.Hybrid module RCAIDE.Framework.Analyses.Weights.Hydrogen module RCAIDE.Framework.Analyses.Weights.Weights module RCAIDE.Framework.Core module RCAIDE.Framework.Core.Arrays module RCAIDE.Framework.Core.Container module RCAIDE.Framework.Core.ContainerOrdered module RCAIDE.Framework.Core.Data module RCAIDE.Framework.Core.DataOrdered module RCAIDE.Framework.Core.Diffed_Data module RCAIDE.Framework.Core.redirect module RCAIDE.Framework.Core.Units module RCAIDE.Framework.Core.Utilities module RCAIDE.Framework.External_Interfaces module RCAIDE.Framework.External_Interfaces.OpenVSP module RCAIDE.Framework.External_Interfaces.OpenVSP.export_vsp_vehicle module RCAIDE.Framework.External_Interfaces.OpenVSP.get_fuel_tank_properties module RCAIDE.Framework.External_Interfaces.OpenVSP.get_vsp_measurements module RCAIDE.Framework.External_Interfaces.OpenVSP.import_vsp_vehicle module RCAIDE.Framework.External_Interfaces.OpenVSP.mach_slices module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_nacelle module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing module RCAIDE.Framework.External_Interfaces.OpenVSP.write_vsp_mesh module RCAIDE.Framework.Mission module RCAIDE.Framework.Mission.Common module RCAIDE.Framework.Mission.Common.Conditions module RCAIDE.Framework.Mission.Common.Numerics module RCAIDE.Framework.Mission.Common.Residuals module RCAIDE.Framework.Mission.Common.Results module RCAIDE.Framework.Mission.Common.State module RCAIDE.Framework.Mission.Common.Unknowns module RCAIDE.Framework.Mission.Missions module RCAIDE.Framework.Mission.Segments module RCAIDE.Framework.Mission.Segments.Climb module RCAIDE.Framework.Mission.Segments.Climb.Constant_CAS_Constant_Rate module RCAIDE.Framework.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle module RCAIDE.Framework.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate module RCAIDE.Framework.Mission.Segments.Climb.Constant_EAS_Constant_Rate module RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Constant_Angle module RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Constant_Rate module RCAIDE.Framework.Mission.Segments.Climb.Constant_Mach_Linear_Altitude module RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Constant_Angle module RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Constant_Rate module RCAIDE.Framework.Mission.Segments.Climb.Constant_Speed_Linear_Altitude module RCAIDE.Framework.Mission.Segments.Climb.Constant_Throttle_Constant_Speed module RCAIDE.Framework.Mission.Segments.Climb.Linear_Mach_Constant_Rate module RCAIDE.Framework.Mission.Segments.Climb.Linear_Speed_Constant_Rate module RCAIDE.Framework.Mission.Segments.Cruise module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter module RCAIDE.Framework.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Cruise.Curved_Constant_Radius_Constant_Speed_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Descent module RCAIDE.Framework.Mission.Segments.Descent.Constant_CAS_Constant_Rate module RCAIDE.Framework.Mission.Segments.Descent.Constant_EAS_Constant_Rate module RCAIDE.Framework.Mission.Segments.Descent.Constant_Speed_Constant_Angle module RCAIDE.Framework.Mission.Segments.Descent.Constant_Speed_Constant_Rate module RCAIDE.Framework.Mission.Segments.Descent.Linear_Mach_Constant_Rate module RCAIDE.Framework.Mission.Segments.Descent.Linear_Speed_Constant_Rate module RCAIDE.Framework.Mission.Segments.Evaluate module RCAIDE.Framework.Mission.Segments.Ground module RCAIDE.Framework.Mission.Segments.Ground.Battery_Discharge module RCAIDE.Framework.Mission.Segments.Ground.Battery_Recharge module RCAIDE.Framework.Mission.Segments.Ground.Ground module RCAIDE.Framework.Mission.Segments.Ground.Landing module RCAIDE.Framework.Mission.Segments.Ground.Takeoff module RCAIDE.Framework.Mission.Segments.Segment module RCAIDE.Framework.Mission.Segments.Single_Point module RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude module RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_AVL_Trimmed module RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion module RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Throttle module RCAIDE.Framework.Mission.Segments.Transition module RCAIDE.Framework.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb module RCAIDE.Framework.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude module RCAIDE.Framework.Mission.Segments.Untrimmed module RCAIDE.Framework.Mission.Segments.Untrimmed.Untrimmed module RCAIDE.Framework.Mission.Segments.Vertical_Flight module RCAIDE.Framework.Mission.Segments.Vertical_Flight.Climb module RCAIDE.Framework.Mission.Segments.Vertical_Flight.Descent module RCAIDE.Framework.Mission.Segments.Vertical_Flight.Hover module RCAIDE.Framework.Mission.Sequential_Segments module RCAIDE.Framework.Networks module RCAIDE.Framework.Networks.Electric module RCAIDE.Framework.Networks.Fuel module RCAIDE.Framework.Networks.Fuel_Cell module RCAIDE.Framework.Networks.Hybrid module RCAIDE.Framework.Networks.Network module RCAIDE.Framework.Optimization module RCAIDE.Framework.Optimization.Common module RCAIDE.Framework.Optimization.Common.helper_functions module RCAIDE.Framework.Optimization.Common.Nexus module RCAIDE.Framework.Optimization.Packages module RCAIDE.Framework.Optimization.Packages.additive module RCAIDE.Framework.Optimization.Packages.additive.additive_setup module RCAIDE.Framework.Optimization.Packages.particle_swarm module RCAIDE.Framework.Optimization.Packages.particle_swarm.particle_swarm_optimization module RCAIDE.Framework.Optimization.Packages.pyopt module RCAIDE.Framework.Optimization.Packages.pyopt.pyopt_setup module RCAIDE.Framework.Optimization.Packages.scipy module RCAIDE.Framework.Optimization.Packages.scipy.scipy_setup module RCAIDE.Framework.Optimization.Packages.trmm module RCAIDE.Framework.Optimization.Packages.trmm.TRMM_setup module RCAIDE.Framework.Optimization.Packages.trmm.Trust_Region module RCAIDE.Framework.Optimization.Packages.trmm.Trust_Region_Optimization module RCAIDE.Library module RCAIDE.Library.Attributes module RCAIDE.Library.Attributes.Atmospheres module RCAIDE.Library.Attributes.Atmospheres.Atmosphere module RCAIDE.Library.Attributes.Atmospheres.Earth module RCAIDE.Library.Attributes.Atmospheres.Earth.Constant_Temperature module RCAIDE.Library.Attributes.Atmospheres.Earth.US_Standard_1976 module RCAIDE.Library.Attributes.Coolants module RCAIDE.Library.Attributes.Coolants.Coolant module RCAIDE.Library.Attributes.Coolants.Glycol_Water module RCAIDE.Library.Attributes.Cryogens module RCAIDE.Library.Attributes.Cryogens.Cryogen module RCAIDE.Library.Attributes.Cryogens.Liquid_Hydrogen module RCAIDE.Library.Attributes.Gases module RCAIDE.Library.Attributes.Gases.Air module RCAIDE.Library.Attributes.Gases.CO2 module RCAIDE.Library.Attributes.Gases.Gas module RCAIDE.Library.Attributes.Gases.Steam module RCAIDE.Library.Attributes.Materials module RCAIDE.Library.Attributes.Materials.Acrylic module RCAIDE.Library.Attributes.Materials.Aluminum module RCAIDE.Library.Attributes.Materials.Aluminum_Alloy module RCAIDE.Library.Attributes.Materials.Bidirectional_Carbon_Fiber module RCAIDE.Library.Attributes.Materials.Carbon_Fiber_Honeycomb module RCAIDE.Library.Attributes.Materials.Copper module RCAIDE.Library.Attributes.Materials.CrossLinked_Polyethylene module RCAIDE.Library.Attributes.Materials.Epoxy module RCAIDE.Library.Attributes.Materials.Magnesium module RCAIDE.Library.Attributes.Materials.Nickel module RCAIDE.Library.Attributes.Materials.Paint module RCAIDE.Library.Attributes.Materials.Perfluoroalkoxy module RCAIDE.Library.Attributes.Materials.Polyetherimide module RCAIDE.Library.Attributes.Materials.Polyimide module RCAIDE.Library.Attributes.Materials.Polytetrafluoroethylene module RCAIDE.Library.Attributes.Materials.Solid module RCAIDE.Library.Attributes.Materials.Steel module RCAIDE.Library.Attributes.Materials.Titanium module RCAIDE.Library.Attributes.Materials.Unidirectional_Carbon_Fiber module RCAIDE.Library.Attributes.Planets module RCAIDE.Library.Attributes.Planets.Earth module RCAIDE.Library.Attributes.Planets.Planet module RCAIDE.Library.Attributes.Propellants module RCAIDE.Library.Attributes.Propellants.Alcohol_Mixture module RCAIDE.Library.Attributes.Propellants.Alkane_Mixture module RCAIDE.Library.Attributes.Propellants.Aviation_Gasoline module RCAIDE.Library.Attributes.Propellants.Butanol module RCAIDE.Library.Attributes.Propellants.Ethane module RCAIDE.Library.Attributes.Propellants.Ethanol module RCAIDE.Library.Attributes.Propellants.Gaseous_Hydrogen module RCAIDE.Library.Attributes.Propellants.Jet_A module RCAIDE.Library.Attributes.Propellants.Jet_A1 module RCAIDE.Library.Attributes.Propellants.JP7 module RCAIDE.Library.Attributes.Propellants.Liquid_Hydrogen module RCAIDE.Library.Attributes.Propellants.Liquid_Natural_Gas module RCAIDE.Library.Attributes.Propellants.Liquid_Petroleum_Gas module RCAIDE.Library.Attributes.Propellants.Methane module RCAIDE.Library.Attributes.Propellants.Propane module RCAIDE.Library.Attributes.Propellants.Propanol module RCAIDE.Library.Attributes.Propellants.Propellant module RCAIDE.Library.Attributes.Propellants.Rocket_LH2 module RCAIDE.Library.Attributes.Propellants.Rocket_RP1 module RCAIDE.Library.Components module RCAIDE.Library.Components.Airfoils module RCAIDE.Library.Components.Airfoils.Airfoil module RCAIDE.Library.Components.Airfoils.Biconvex_Airfoil module RCAIDE.Library.Components.Airfoils.NACA_4_Series_Airfoil module RCAIDE.Library.Components.Booms module RCAIDE.Library.Components.Booms.Boom module RCAIDE.Library.Components.Component module RCAIDE.Library.Components.Configs module RCAIDE.Library.Components.Configs.Config module RCAIDE.Library.Components.Fuselages module RCAIDE.Library.Components.Fuselages.Blended_Wing_Body_Fuselage module RCAIDE.Library.Components.Fuselages.Cabins module RCAIDE.Library.Components.Fuselages.Cabins.Cabin module RCAIDE.Library.Components.Fuselages.Cabins.Classes module RCAIDE.Library.Components.Fuselages.Cabins.Classes.Business module RCAIDE.Library.Components.Fuselages.Cabins.Classes.Economy module RCAIDE.Library.Components.Fuselages.Cabins.Classes.First module RCAIDE.Library.Components.Fuselages.Cabins.Side_Cabin module RCAIDE.Library.Components.Fuselages.Fuselage module RCAIDE.Library.Components.Fuselages.Segments module RCAIDE.Library.Components.Fuselages.Segments.Circle_Segment module RCAIDE.Library.Components.Fuselages.Segments.Ellipse_Segment module RCAIDE.Library.Components.Fuselages.Segments.Rounded_Rectangle_Segment module RCAIDE.Library.Components.Fuselages.Segments.Segment module RCAIDE.Library.Components.Fuselages.Segments.Super_Ellipse_Segment module RCAIDE.Library.Components.Fuselages.Tube_Fuselage module RCAIDE.Library.Components.Landing_Gear module RCAIDE.Library.Components.Landing_Gear.Landing_Gear module RCAIDE.Library.Components.Landing_Gear.Main_Landing_Gear module RCAIDE.Library.Components.Landing_Gear.Nose_Landing_Gear module RCAIDE.Library.Components.Mass_Properties module RCAIDE.Library.Components.Nacelles module RCAIDE.Library.Components.Nacelles.Body_of_Revolution_Nacelle module RCAIDE.Library.Components.Nacelles.Nacelle module RCAIDE.Library.Components.Nacelles.Segments module RCAIDE.Library.Components.Nacelles.Segments.Segment module RCAIDE.Library.Components.Nacelles.Stack_Nacelle module RCAIDE.Library.Components.Network module RCAIDE.Library.Components.Payloads module RCAIDE.Library.Components.Payloads.Payload module RCAIDE.Library.Components.Powertrain module RCAIDE.Library.Components.Powertrain.Converters module RCAIDE.Library.Components.Powertrain.Converters.Combustor module RCAIDE.Library.Components.Powertrain.Converters.Compression_Nozzle module RCAIDE.Library.Components.Powertrain.Converters.Compressor module RCAIDE.Library.Components.Powertrain.Converters.Converter module RCAIDE.Library.Components.Powertrain.Converters.DC_Generator module RCAIDE.Library.Components.Powertrain.Converters.DC_Motor module RCAIDE.Library.Components.Powertrain.Converters.Ducted_Fan module RCAIDE.Library.Components.Powertrain.Converters.Engine module RCAIDE.Library.Components.Powertrain.Converters.Expansion_Nozzle module RCAIDE.Library.Components.Powertrain.Converters.Fan module RCAIDE.Library.Components.Powertrain.Converters.Generic_Fuel_Cell_Stack module RCAIDE.Library.Components.Powertrain.Converters.Lift_Rotor module RCAIDE.Library.Components.Powertrain.Converters.PMSM_Generator module RCAIDE.Library.Components.Powertrain.Converters.PMSM_Motor module RCAIDE.Library.Components.Powertrain.Converters.Prop_Rotor module RCAIDE.Library.Components.Powertrain.Converters.Propeller module RCAIDE.Library.Components.Powertrain.Converters.Proton_Exchange_Membrane_Fuel_Cell module RCAIDE.Library.Components.Powertrain.Converters.Ram module RCAIDE.Library.Components.Powertrain.Converters.Reformer module RCAIDE.Library.Components.Powertrain.Converters.Rotor module RCAIDE.Library.Components.Powertrain.Converters.Supersonic_Nozzle module RCAIDE.Library.Components.Powertrain.Converters.Turbine module RCAIDE.Library.Components.Powertrain.Converters.Turboelectric_Generator module RCAIDE.Library.Components.Powertrain.Converters.Turboshaft module RCAIDE.Library.Components.Powertrain.Distributors module RCAIDE.Library.Components.Powertrain.Distributors.Coolant_Line module RCAIDE.Library.Components.Powertrain.Distributors.Electrical_Bus module RCAIDE.Library.Components.Powertrain.Distributors.Fuel_Line module RCAIDE.Library.Components.Powertrain.Modulators module RCAIDE.Library.Components.Powertrain.Modulators.Electronic_Speed_Controller module RCAIDE.Library.Components.Powertrain.Modulators.Fuel_Selector module RCAIDE.Library.Components.Powertrain.Propulsors module RCAIDE.Library.Components.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine module RCAIDE.Library.Components.Powertrain.Propulsors.Electric_Ducted_Fan module RCAIDE.Library.Components.Powertrain.Propulsors.Electric_Rotor module RCAIDE.Library.Components.Powertrain.Propulsors.Internal_Combustion_Engine module RCAIDE.Library.Components.Powertrain.Propulsors.Propulsor module RCAIDE.Library.Components.Powertrain.Propulsors.Turbofan module RCAIDE.Library.Components.Powertrain.Propulsors.Turbojet module RCAIDE.Library.Components.Powertrain.Propulsors.Turboprop module RCAIDE.Library.Components.Powertrain.Sources module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Aluminum_Air module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Generic_Battery_Module module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Air module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_LFP module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Ion_NMC module RCAIDE.Library.Components.Powertrain.Sources.Battery_Modules.Lithium_Sulfur module RCAIDE.Library.Components.Powertrain.Sources.Cryogenic_Tanks module RCAIDE.Library.Components.Powertrain.Sources.Cryogenic_Tanks.Cryogenic_Tank module RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks module RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks.Central_Fuel_Tank module RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks.Fuel_Tank module RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks.Wing_Fuel_Tank module RCAIDE.Library.Components.Powertrain.Systems module RCAIDE.Library.Components.Powertrain.Systems.Avionics module RCAIDE.Library.Components.Powertrain.Systems.System module RCAIDE.Library.Components.Thermal_Management module RCAIDE.Library.Components.Thermal_Management.Accessories module RCAIDE.Library.Components.Thermal_Management.Accessories.Fan module RCAIDE.Library.Components.Thermal_Management.Accessories.Pump module RCAIDE.Library.Components.Thermal_Management.Batteries module RCAIDE.Library.Components.Thermal_Management.Batteries.Air_Cooled module RCAIDE.Library.Components.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel module RCAIDE.Library.Components.Thermal_Management.Heat_Exchangers module RCAIDE.Library.Components.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger module RCAIDE.Library.Components.Thermal_Management.Reservoirs module RCAIDE.Library.Components.Thermal_Management.Reservoirs.Reservoir module RCAIDE.Library.Components.Wings module RCAIDE.Library.Components.Wings.All_Moving_Surface module RCAIDE.Library.Components.Wings.Control_Surfaces module RCAIDE.Library.Components.Wings.Control_Surfaces.Aileron module RCAIDE.Library.Components.Wings.Control_Surfaces.Control_Surface module RCAIDE.Library.Components.Wings.Control_Surfaces.Elevator module RCAIDE.Library.Components.Wings.Control_Surfaces.Flap module RCAIDE.Library.Components.Wings.Control_Surfaces.Rudder module RCAIDE.Library.Components.Wings.Control_Surfaces.Slat module RCAIDE.Library.Components.Wings.Control_Surfaces.Spoiler module RCAIDE.Library.Components.Wings.Horizontal_Tail module RCAIDE.Library.Components.Wings.Main_Wing module RCAIDE.Library.Components.Wings.Segments module RCAIDE.Library.Components.Wings.Segments.Segment module RCAIDE.Library.Components.Wings.Stabilator module RCAIDE.Library.Components.Wings.Vertical_Tail module RCAIDE.Library.Components.Wings.Vertical_Tail_All_Moving module RCAIDE.Library.Components.Wings.Wing module RCAIDE.Library.Methods module RCAIDE.Library.Methods.Aerodynamics module RCAIDE.Library.Methods.Aerodynamics.AERODAS module RCAIDE.Library.Methods.Aerodynamics.AERODAS.post_stall_coefficients module RCAIDE.Library.Methods.Aerodynamics.AERODAS.pre_stall_coefficients module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.aero_coeff module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.airfoil_analysis module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.cf_filter module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.chordwise_distribution module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.heads_method module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.hess_smith module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.infl_coeff module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.panel_geometry module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.velocity_distribution module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Aircraft module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Body module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Configuration module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Inputs module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Run_Case module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.build_AVL_surrogates module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.evaluate_AVL module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.purge_files module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.read_results module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.run_AVL_analysis module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.train_AVL_surrogates module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.translate_data module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_avl_airfoil_file module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_mass_file module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_run_cases module RCAIDE.Library.Methods.Aerodynamics.Common module RCAIDE.Library.Methods.Aerodynamics.Common.Drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.asymmetry_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressibility_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressible_mixed_flat_plate module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressible_turbulent_flat_plate module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.cooling_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.drag_divergence module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.estimate_2ndseg_lift_drag_ratio module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.induced_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.lift_wave_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.miscellaneous_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_fuselage module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_nacelle module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_pylon module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_drag_wing module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_total module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.spoiler_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.supersonic_wave_drag_volume_raymer module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.supersonic_wave_drag_volume_sears_haack module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.total_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.wave_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.wave_drag_lift module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.windmilling_drag module RCAIDE.Library.Methods.Aerodynamics.Common.Lift module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.BET_calculations module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_flap_lift module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_max_lift_coeff module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_slat_lift module RCAIDE.Library.Methods.Aerodynamics.Common.Lift.fuselage_correction module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.build_VLM_surrogates module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_RHS_matrix module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_wing_induced_velocity module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.evaluate_VLM module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.extract_wing_collocation_points module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_VD_helpers module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.generate_vortex_distribution module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.train_VLM_surrogates module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.VLM module RCAIDE.Library.Methods.Emissions module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.build_CRN_EI_surrogates module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_cantera module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.evaluate_CRN_emission_indices module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.train_CRN_EI_surrogates module RCAIDE.Library.Methods.Emissions.Emission_Index_Empirical_Method module RCAIDE.Library.Methods.Emissions.Emission_Index_Empirical_Method.evaluate_correlation_emissions_indices module RCAIDE.Library.Methods.Gas_Dynamics module RCAIDE.Library.Methods.Gas_Dynamics.fm_id module RCAIDE.Library.Methods.Geodesics module RCAIDE.Library.Methods.Geodesics.compute_point_to_point_geospacial_data module RCAIDE.Library.Methods.Geodesics.Geodesics module RCAIDE.Library.Methods.Geometry module RCAIDE.Library.Methods.Geometry.Airfoil module RCAIDE.Library.Methods.Geometry.Airfoil.compute_airfoil_properties module RCAIDE.Library.Methods.Geometry.Airfoil.compute_naca_4series module RCAIDE.Library.Methods.Geometry.Airfoil.convert_airfoil_to_meshgrid module RCAIDE.Library.Methods.Geometry.Airfoil.generate_interpolated_airfoils module RCAIDE.Library.Methods.Geometry.Airfoil.import_airfoil_dat module RCAIDE.Library.Methods.Geometry.Airfoil.import_airfoil_geometry module RCAIDE.Library.Methods.Geometry.Airfoil.import_airfoil_polars module RCAIDE.Library.Methods.Geometry.LOPA module RCAIDE.Library.Methods.Geometry.LOPA.compute_layout_of_passenger_accommodations module RCAIDE.Library.Methods.Geometry.LOPA.LOPA_functions module RCAIDE.Library.Methods.Geometry.Planform module RCAIDE.Library.Methods.Geometry.Planform.compute_chord_length_from_span_location module RCAIDE.Library.Methods.Geometry.Planform.compute_span_location_from_chord_length module RCAIDE.Library.Methods.Geometry.Planform.convert_sweep module RCAIDE.Library.Methods.Geometry.Planform.estimate_wing_internal_volume module RCAIDE.Library.Methods.Geometry.Planform.fuselage_planform module RCAIDE.Library.Methods.Geometry.Planform.horizontal_tail_planform module RCAIDE.Library.Methods.Geometry.Planform.horizontal_tail_planform_raymer module RCAIDE.Library.Methods.Geometry.Planform.populate_control_sections module RCAIDE.Library.Methods.Geometry.Planform.vertical_tail_planform module RCAIDE.Library.Methods.Geometry.Planform.vertical_tail_planform_raymer module RCAIDE.Library.Methods.Geometry.Planform.wing_fuel_volume module RCAIDE.Library.Methods.Geometry.Planform.wing_planform module RCAIDE.Library.Methods.Geometry.Planform.wing_segmented_planform module RCAIDE.Library.Methods.Mass_Properties module RCAIDE.Library.Methods.Mass_Properties.Center_of_Gravity module RCAIDE.Library.Methods.Mass_Properties.Center_of_Gravity.compute_component_centers_of_gravity module RCAIDE.Library.Methods.Mass_Properties.Center_of_Gravity.compute_vehicle_center_of_gravity module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_aircraft_moment_of_inertia module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_cuboid_moment_of_inertia module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_cylinder_moment_of_inertia module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_fuselage_moment_of_inertia module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_wing_moment_of_inertia module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.mass_and_intertia_functions module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_aft_centerbody_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_cabin_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Common module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Common.compute_payload_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_fuselage_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_horizontal_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_landing_gear_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_operating_items_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_propulsion_system_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_systems_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_vertical_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_fuselage_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_horizontal_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_landing_gear_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_main_wing_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_payload_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_propulsion_system_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_systems_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer.compute_vertical_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Common module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Common.compute_operating_items_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_fuselage_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_horizontal_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_landing_gear_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_operating_items_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_propulsion_system_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_systems_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_vertical_tail_weight module

RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_fuselage_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_horizontal_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_landing_gear_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_main_wing_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_propulsion_system_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_systems_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.Raymer.compute_vertical_tail_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_motor_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_rotor_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_wiring_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.General_Aviation module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.General_Aviation.Physics_Based module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.General_Aviation.Physics_Based.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_boom_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_fuselage_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_operating_empty_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.compute_wing_weight module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.VTOL.Physics_Based.dynamo_supply_mass_estimation module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Hybrid module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Hydrogen module RCAIDE.Library.Methods.Noise module RCAIDE.Library.Methods.Noise.Boom module RCAIDE.Library.Methods.Noise.Boom.lift_equivalent_area module RCAIDE.Library.Methods.Noise.Common module RCAIDE.Library.Methods.Noise.Common.atmospheric_attenuation module RCAIDE.Library.Methods.Noise.Common.background_noise module RCAIDE.Library.Methods.Noise.Common.compute_noise_source_coordinates module RCAIDE.Library.Methods.Noise.Common.compute_relative_noise_evaluation_locations module RCAIDE.Library.Methods.Noise.Common.convert_to_third_octave_band module RCAIDE.Library.Methods.Noise.Common.decibel_arithmetic module RCAIDE.Library.Methods.Noise.Common.generate_hemisphere_microphone_locations module RCAIDE.Library.Methods.Noise.Common.generate_terrain_microphone_locations module RCAIDE.Library.Methods.Noise.Common.generate_zero_elevation_microphone_locations module RCAIDE.Library.Methods.Noise.Correlation_Buildup module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.airframe_noise module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.clean_wing_noise module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.landing_gear_noise module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.trailing_edge_flap_noise module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.angle_of_attack_effect module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.external_plug_effect module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.ground_proximity_effect module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.jet_installation_effect module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.mixed_noise_component module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.noise_source_location module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.primary_noise_component module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.secondary_noise_component module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.turbofan_engine_noise module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.BPM_boundary_layer_properties module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.broadband_noise module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.compute_rotor_noise module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.harmonic_noise_line module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.harmonic_noise_plane module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.harmonic_noise_point module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.LBL_VS_broadband_noise module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.noise_directivities module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TIP_broadband_noise module RCAIDE.Library.Methods.Noise.Metrics module RCAIDE.Library.Methods.Noise.Metrics.A_weighting_metric module RCAIDE.Library.Methods.Noise.Metrics.EPNL_noise_metric module RCAIDE.Library.Methods.Noise.Metrics.Equivalent_SENEL_SEL_noise_metrics module RCAIDE.Library.Methods.Noise.Metrics.PNL_noise_metric module RCAIDE.Library.Methods.Performance module RCAIDE.Library.Methods.Performance.aircraft_aerodynamic_analysis module RCAIDE.Library.Methods.Performance.compute_noise_certification_data module RCAIDE.Library.Methods.Performance.compute_payload_range_diagram module RCAIDE.Library.Methods.Performance.estimate_landing_field_length module RCAIDE.Library.Methods.Performance.estimate_stall_speed module RCAIDE.Library.Methods.Performance.estimate_take_off_field_length module RCAIDE.Library.Methods.Performance.find_take_off_weight_given_tofl module RCAIDE.Library.Methods.Performance.generate_V_n_diagram module RCAIDE.Library.Methods.Performance.propeller_aerodynamic_analysis module RCAIDE.Library.Methods.Performance.rotor_aerodynamic_analysis module RCAIDE.Library.Methods.Powertrain module RCAIDE.Library.Methods.Powertrain.Converters module RCAIDE.Library.Methods.Powertrain.Converters.Combustor module RCAIDE.Library.Methods.Powertrain.Converters.Combustor.append_combustor_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Combustor.compute_combustor_performance module RCAIDE.Library.Methods.Powertrain.Converters.Compression_Nozzle module RCAIDE.Library.Methods.Powertrain.Converters.Compression_Nozzle.append_compression_nozzle_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Compression_Nozzle.compute_compression_nozzle_performance module RCAIDE.Library.Methods.Powertrain.Converters.Compressor module RCAIDE.Library.Methods.Powertrain.Converters.Compressor.append_compressor_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Compressor.compute_compressor_performance module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.append_ducted_fan_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.compute_ducted_fan_performance module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.design_ducted_fan module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.BEMT_performance module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.purge_files module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.read_results module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.run_dfdc_analysis module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.translate_conditions_to_dfdc_cases module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_geometry module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_input_deck module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Rankine_Froude_Momentum_Theory module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Rankine_Froude_Momentum_Theory.RFMT_performance module RCAIDE.Library.Methods.Powertrain.Converters.Engine module RCAIDE.Library.Methods.Powertrain.Converters.Engine.append_engine_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Engine.compute_power_from_throttle module RCAIDE.Library.Methods.Powertrain.Converters.Engine.compute_throttle_from_power module RCAIDE.Library.Methods.Powertrain.Converters.Expansion_Nozzle module RCAIDE.Library.Methods.Powertrain.Converters.Expansion_Nozzle.append_expansion_nozzle_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Expansion_Nozzle.compute_expansion_nozzle_performance module RCAIDE.Library.Methods.Powertrain.Converters.Fan module RCAIDE.Library.Methods.Powertrain.Converters.Fan.append_fan_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Fan.compute_fan_performance module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Common module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Common.compute_stack_properties module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.append_fuel_cell_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_fuel_cell_performance module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_power module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_power_difference module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.compute_voltage module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.append_fuel_cell_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance module RCAIDE.Library.Methods.Powertrain.Converters.Generator module RCAIDE.Library.Methods.Powertrain.Converters.Generator.append_generator_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Generator.compute_generator_performance module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator module RCAIDE.Library.Methods.Powertrain.Converters.Motor module RCAIDE.Library.Methods.Powertrain.Converters.Motor.append_motor_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Motor.compute_motor_performance module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor module RCAIDE.Library.Methods.Powertrain.Converters.Ram module RCAIDE.Library.Methods.Powertrain.Converters.Ram.append_ram_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Ram.compute_ram_performance module RCAIDE.Library.Methods.Powertrain.Converters.Reformer module RCAIDE.Library.Methods.Powertrain.Converters.Reformer.compute_reformer_performance module RCAIDE.Library.Methods.Powertrain.Converters.Rotor module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.append_rotor_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.compute_rotor_performance module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.blade_geometry_setup module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.optimization_setup module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.set_optimized_parameters module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_lift_rotor module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_prop_rotor module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.design_propeller module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Actuator_Disc_Theory module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Actuator_Disc_Theory.Actuator_Disk_performance module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.BEMT_Helmholtz_performance module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.compute_wake_contraction_matrix module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.compute_wake_induced_velocity module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model module RCAIDE.Library.Methods.Powertrain.Converters.Supersonic_Nozzle module RCAIDE.Library.Methods.Powertrain.Converters.Supersonic_Nozzle.append_supersonic_nozzle_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Supersonic_Nozzle.compute_supersonic_nozzle_performance module RCAIDE.Library.Methods.Powertrain.Converters.Turbine module RCAIDE.Library.Methods.Powertrain.Converters.Turbine.append_turbine_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Turbine.compute_turbine_performance module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.append_turboelectric_generator_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.compute_turboelectric_generator_performance module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.design_turboelectric_generator module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.append_turboshaft_conditions module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.compute_power module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.compute_turboshaft_performance module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.design_turboshaft module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.size_core module RCAIDE.Library.Methods.Powertrain.Distributors module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.append_bus_conditions module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.compute_bus_conditions module RCAIDE.Library.Methods.Powertrain.Distributors.Electrical_Bus.initialize_bus_properties module RCAIDE.Library.Methods.Powertrain.Modulators module RCAIDE.Library.Methods.Powertrain.Modulators.Electronic_Speed_Controller module RCAIDE.Library.Methods.Powertrain.Modulators.Electronic_Speed_Controller.append_esc_conditions module RCAIDE.Library.Methods.Powertrain.Modulators.Electronic_Speed_Controller.compute_esc_performance module RCAIDE.Library.Methods.Powertrain.Propulsors module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.append_constant_speed_internal_combustion_engine_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.compute_constant_speed_internal_combustion_engine_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.design_constant_speed_internal_combustion_engine module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.append_electric_ducted_fan_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.append_electric_ducted_fan_residual_and_unknown module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.compute_electric_ducted_fan_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.design_electric_ducted_fan module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.pack_electric_ducted_fan_residuals module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.unpack_electric_ducted_fan_unknowns module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.append_electric_rotor_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.append_electric_rotor_residual_and_unknown module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.compute_electric_rotor_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.design_electric_rotor module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.pack_electric_rotor_residuals module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.unpack_electric_rotor_unknowns module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.append_internal_combustion_engine_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.append_internal_combustion_engine_residual_and_unknown module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.compute_internal_combustion_engine_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.design_internal_combustion_engine module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.pack_internal_combustion_engine_residuals module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.unpack_internal_combustion_engine_unknowns module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.append_turbofan_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.compute_thurst module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.compute_turbofan_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.design_turbofan module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.size_core module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.append_turbojet_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_thurst module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_turbojet_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.design_turbojet module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.size_core module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.append_turboprop_conditions module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_thrust module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_turboprop_performance module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.design_turboprop module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.size_core module RCAIDE.Library.Methods.Powertrain.setup_operating_conditions module RCAIDE.Library.Methods.Powertrain.Sources module RCAIDE.Library.Methods.Powertrain.Sources.Batteries module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Aluminum_Air module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Aluminum_Air.compute_al_air_cell_performance module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.append_battery_conditions module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.compute_module_properties module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_mass_gain_rate module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_ragone_properties module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_specific_power module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.find_total_mass_gain module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.size_module_from_energy_and_power module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.size_module_from_mass module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.compute_lfp_cell_performance module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.update_lfp_cell_age module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.compute_nmc_cell_performance module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.update_nmc_cell_age module RCAIDE.Library.Methods.Powertrain.Sources.Cryogenic_Tanks module RCAIDE.Library.Methods.Powertrain.Sources.Cryogenic_Tanks.append_cryogenic_tank_conditions module RCAIDE.Library.Methods.Powertrain.Sources.Fuel_Tanks module RCAIDE.Library.Methods.Powertrain.Sources.Fuel_Tanks.append_fuel_tank_conditions module RCAIDE.Library.Methods.Powertrain.Systems module RCAIDE.Library.Methods.Powertrain.Systems.append_avionics_conditions module RCAIDE.Library.Methods.Powertrain.Systems.append_payload_conditions module RCAIDE.Library.Methods.Powertrain.Systems.compute_avionics_power_draw module RCAIDE.Library.Methods.Powertrain.Systems.compute_payload_power_draw module RCAIDE.Library.Methods.skip module RCAIDE.Library.Methods.Stability module RCAIDE.Library.Methods.Stability.compute_dynamic_flight_modes module RCAIDE.Library.Methods.Thermal_Management module RCAIDE.Library.Methods.Thermal_Management.Batteries module RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled module RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.air_cooled_performance module RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.append_air_cooled_conditions module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.append_wavy_channel_conditions module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.design_wavy_channel module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_geometry_setup module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_rating_model module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_sizing_setup module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.append_cross_flow_heat_exchanger_conditions module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.compute_heat_exhanger_factors module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_geometry_setup module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_heat_exchanger_sizing_setup module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.cross_flow_hex_rating_model module RCAIDE.Library.Methods.Thermal_Management.Heat_Exchangers.Cross_Flow_Heat_Exchanger.design_cross_flow_heat_exchanger module RCAIDE.Library.Methods.Thermal_Management.Reservoirs module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.append_reservoir_conditions module RCAIDE.Library.Methods.Thermal_Management.Reservoirs.Reservoir_Tank.compute_mixing_temperature module RCAIDE.Library.Methods.Utilities module RCAIDE.Library.Methods.Utilities.Chebyshev module RCAIDE.Library.Methods.Utilities.Chebyshev.chebyshev_data module RCAIDE.Library.Methods.Utilities.Chebyshev.linear_data module RCAIDE.Library.Methods.Utilities.Cubic_Spline_Blender module RCAIDE.Library.Methods.Utilities.latin_hypercube_sampling module RCAIDE.Library.Mission module RCAIDE.Library.Mission.Common module RCAIDE.Library.Mission.Common.Initialize module RCAIDE.Library.Mission.Common.Initialize.differentials_altitude module RCAIDE.Library.Mission.Common.Initialize.differentials_dimensionless module RCAIDE.Library.Mission.Common.Initialize.energy module RCAIDE.Library.Mission.Common.Initialize.inertial_position module RCAIDE.Library.Mission.Common.Initialize.planet_position module RCAIDE.Library.Mission.Common.Initialize.time module RCAIDE.Library.Mission.Common.Initialize.weights module RCAIDE.Library.Mission.Common.Pre_Process module RCAIDE.Library.Mission.Common.Pre_Process.aerodynamics module RCAIDE.Library.Mission.Common.Pre_Process.emissions module RCAIDE.Library.Mission.Common.Pre_Process.energy module RCAIDE.Library.Mission.Common.Pre_Process.mass_properties module RCAIDE.Library.Mission.Common.Pre_Process.set_residuals_and_unknowns module RCAIDE.Library.Mission.Common.Pre_Process.stability module RCAIDE.Library.Mission.Common.Residuals module RCAIDE.Library.Mission.Common.Residuals.flight_dynamics module RCAIDE.Library.Mission.Common.Segments module RCAIDE.Library.Mission.Common.Unpack_Unknowns module RCAIDE.Library.Mission.Common.Unpack_Unknowns.control_surfaces module RCAIDE.Library.Mission.Common.Unpack_Unknowns.energy module RCAIDE.Library.Mission.Common.Unpack_Unknowns.ground module RCAIDE.Library.Mission.Common.Unpack_Unknowns.orientation module RCAIDE.Library.Mission.Common.Update module RCAIDE.Library.Mission.Common.Update.acceleration module RCAIDE.Library.Mission.Common.Update.aerodynamics module RCAIDE.Library.Mission.Common.Update.altitude module RCAIDE.Library.Mission.Common.Update.angular_acceleration module RCAIDE.Library.Mission.Common.Update.atmosphere module RCAIDE.Library.Mission.Common.Update.curvilinear_inertial_horizontal_position module RCAIDE.Library.Mission.Common.Update.differentials_time module RCAIDE.Library.Mission.Common.Update.emissions module RCAIDE.Library.Mission.Common.Update.energy module RCAIDE.Library.Mission.Common.Update.forces module RCAIDE.Library.Mission.Common.Update.freestream module RCAIDE.Library.Mission.Common.Update.gravity module RCAIDE.Library.Mission.Common.Update.ground_forces module RCAIDE.Library.Mission.Common.Update.kinematics module RCAIDE.Library.Mission.Common.Update.linear_inertial_horizontal_position module RCAIDE.Library.Mission.Common.Update.moments module RCAIDE.Library.Mission.Common.Update.noise module RCAIDE.Library.Mission.Common.Update.orientations module RCAIDE.Library.Mission.Common.Update.planet_position module RCAIDE.Library.Mission.Common.Update.stability module RCAIDE.Library.Mission.Common.Update.thrust module RCAIDE.Library.Mission.Common.Update.weights module RCAIDE.Library.Mission.Segments module RCAIDE.Library.Mission.Segments.Climb module RCAIDE.Library.Mission.Segments.Climb.Constant_CAS_Constant_Rate module RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle module RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Rate module RCAIDE.Library.Mission.Segments.Climb.Constant_EAS_Constant_Rate module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Angle module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Rate module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Linear_Altitude module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Angle_Noise module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Constant_Rate module RCAIDE.Library.Mission.Segments.Climb.Constant_Speed_Linear_Altitude module RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed module RCAIDE.Library.Mission.Segments.Climb.Linear_Mach_Constant_Rate module RCAIDE.Library.Mission.Segments.Climb.Linear_Speed_Constant_Rate module RCAIDE.Library.Mission.Segments.Cruise module RCAIDE.Library.Mission.Segments.Cruise.Constant_Acceleration_Constant_Altitude module RCAIDE.Library.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude module RCAIDE.Library.Mission.Segments.Cruise.Constant_Dynamic_Pressure_Constant_Altitude_Loiter module RCAIDE.Library.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude module RCAIDE.Library.Mission.Segments.Cruise.Constant_Mach_Constant_Altitude_Loiter module RCAIDE.Library.Mission.Segments.Cruise.Constant_Pitch_Rate_Constant_Altitude module RCAIDE.Library.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude module RCAIDE.Library.Mission.Segments.Cruise.Constant_Speed_Constant_Altitude_Loiter module RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude module RCAIDE.Library.Mission.Segments.Cruise.Curved_Constant_Radius_Constant_Speed_Constant_Altitude module RCAIDE.Library.Mission.Segments.Descent module RCAIDE.Library.Mission.Segments.Descent.Constant_CAS_Constant_Rate module RCAIDE.Library.Mission.Segments.Descent.Constant_EAS_Constant_Rate module RCAIDE.Library.Mission.Segments.Descent.Constant_Speed_Constant_Angle module RCAIDE.Library.Mission.Segments.Descent.Constant_Speed_Constant_Rate module RCAIDE.Library.Mission.Segments.Descent.Linear_Mach_Constant_Rate module RCAIDE.Library.Mission.Segments.Descent.Linear_Speed_Constant_Rate module RCAIDE.Library.Mission.Segments.Ground module RCAIDE.Library.Mission.Segments.Ground.Battery_Charge_Discharge module RCAIDE.Library.Mission.Segments.Ground.Landing module RCAIDE.Library.Mission.Segments.Ground.Takeoff module RCAIDE.Library.Mission.Segments.Single_Point module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_AVL_Trimmed module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Throttle module RCAIDE.Library.Mission.Segments.Transition module RCAIDE.Library.Mission.Segments.Transition.Constant_Acceleration_Constant_Angle_Linear_Climb module RCAIDE.Library.Mission.Segments.Transition.Constant_Acceleration_Constant_Pitchrate_Constant_Altitude module RCAIDE.Library.Mission.Segments.Untrimmed module RCAIDE.Library.Mission.Segments.Untrimmed.Untrimmed module RCAIDE.Library.Mission.Segments.Vertical_Flight module RCAIDE.Library.Mission.Segments.Vertical_Flight.Climb module RCAIDE.Library.Mission.Segments.Vertical_Flight.Descent module RCAIDE.Library.Mission.Segments.Vertical_Flight.Hover module RCAIDE.Library.Mission.Solver module RCAIDE.Library.Mission.Solver.converge module RCAIDE.Library.Mission.Solver.expand_state module RCAIDE.Library.Plots module RCAIDE.Library.Plots.Aerodynamics module RCAIDE.Library.Plots.Aerodynamics.plot_aerodynamic_coefficients module RCAIDE.Library.Plots.Aerodynamics.plot_aerodynamic_forces module RCAIDE.Library.Plots.Aerodynamics.plot_aircraft_aerodynamics module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_boundary_layer_properties module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_polar_files module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_polars module RCAIDE.Library.Plots.Aerodynamics.plot_airfoil_surface_forces module RCAIDE.Library.Plots.Aerodynamics.plot_disc_and_power_loading module RCAIDE.Library.Plots.Aerodynamics.plot_drag_components module RCAIDE.Library.Plots.Aerodynamics.plot_lift_distribution module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_conditions module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_disc_performance module RCAIDE.Library.Plots.Aerodynamics.plot_rotor_performance module RCAIDE.Library.Plots.Aerodynamics.plot_surface_pressures module RCAIDE.Library.Plots.Common module RCAIDE.Library.Plots.Emissions module RCAIDE.Library.Plots.Emissions.plot_CO2e_emissions module RCAIDE.Library.Plots.Energy module RCAIDE.Library.Plots.Energy.plot_altitude_sfc_weight module RCAIDE.Library.Plots.Energy.plot_battery_cell_conditions module RCAIDE.Library.Plots.Energy.plot_battery_degradation module RCAIDE.Library.Plots.Energy.plot_battery_module_C_rates module RCAIDE.Library.Plots.Energy.plot_battery_module_conditions module RCAIDE.Library.Plots.Energy.plot_battery_pack_conditions module RCAIDE.Library.Plots.Energy.plot_battery_ragone_diagram module RCAIDE.Library.Plots.Energy.plot_battery_temperature module RCAIDE.Library.Plots.Energy.plot_crogenic_fuel_consumption module RCAIDE.Library.Plots.Energy.plot_electric_propulsor_efficiencies module RCAIDE.Library.Plots.Energy.plot_fuel_consumption module RCAIDE.Library.Plots.Energy.plot_propulsor_throttles module RCAIDE.Library.Plots.Geometry module RCAIDE.Library.Plots.Geometry.Common module RCAIDE.Library.Plots.Geometry.Common.contour_surface_slice module RCAIDE.Library.Plots.Geometry.plot_3d_fuselage module RCAIDE.Library.Plots.Geometry.plot_3d_nacelle module RCAIDE.Library.Plots.Geometry.plot_3d_rotor module RCAIDE.Library.Plots.Geometry.plot_3d_vehicle module RCAIDE.Library.Plots.Geometry.plot_3d_vehicle_vlm_panelization module RCAIDE.Library.Plots.Geometry.plot_3d_wing module RCAIDE.Library.Plots.Geometry.plot_airfoil module RCAIDE.Library.Plots.Geometry.plot_layout_of_passenger_accommodations module RCAIDE.Library.Plots.Geometry.plot_rotor module RCAIDE.Library.Plots.Mission module RCAIDE.Library.Plots.Mission.plot_aircraft_velocities module RCAIDE.Library.Plots.Mission.plot_flight_conditions module RCAIDE.Library.Plots.Mission.plot_flight_trajectory module RCAIDE.Library.Plots.Noise module RCAIDE.Library.Plots.Noise.plot_2D_noise_contour module RCAIDE.Library.Plots.Noise.plot_3D_noise_contour module RCAIDE.Library.Plots.Noise.plot_noise_level module RCAIDE.Library.Plots.Noise.post_process_noise_data module RCAIDE.Library.Plots.Stability module RCAIDE.Library.Plots.Stability.plot_flight_forces_and_moments module RCAIDE.Library.Plots.Stability.plot_lateral_stability module RCAIDE.Library.Plots.Stability.plot_longitudinal_stability module RCAIDE.Library.Plots.Thermal_Management module RCAIDE.Library.Plots.Thermal_Management.plot_air_cooled_conditions module RCAIDE.Library.Plots.Thermal_Management.plot_cross_flow_heat_exchanger_conditions module RCAIDE.Library.Plots.Thermal_Management.plot_reservoir_conditions module RCAIDE.Library.Plots.Thermal_Management.plot_thermal_management_performance module RCAIDE.Library.Plots.Thermal_Management.plot_wavy_channel_conditions module RCAIDE.Library.Plots.Topography module RCAIDE.Library.Plots.Topography.plot_elevation_contours module RCAIDE.Library.Plots.Weights module RCAIDE.Library.Plots.Weights.plot_weight_breakdown module RCAIDE.load module RCAIDE.save module RCAIDE.Vehicle module Re_airgap (PMSM_Motor attribute) Re_cooling_flow (PMSM_Motor attribute) reactant (Alcohol_Mixture attribute) (Alkane_Mixture attribute) (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Gaseous_Hydrogen attribute) (Jet_A attribute) (Jet_A1 attribute) (JP7 attribute) (Liquid_Hydrogen attribute) (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Methane attribute) (Propane attribute) (Propanol attribute) (Propellant attribute) read_RCAIDE_json_dict() (in module RCAIDE.load) read_results() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.read_results) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.read_results) read_vsp_boom() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom), [1] read_vsp_fuselage() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] read_vsp_nacelle() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_nacelle), [1] read_vsp_rotor() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor), [1] read_vsp_wing() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing), [1] recursive_set() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) REDUCEDLENGTH (Geodesic attribute), [1] (GeodesicCapability attribute), [1] reference_pressure (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) reference_temperature (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) Reformer (class in RCAIDE.Library.Components.Powertrain.Converters.Reformer) remainder() (Math static method), [1] reprocess_span_breaks() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.make_VLM_wings) Reservoir (class in RCAIDE.Library.Components.Thermal_Management.Reservoirs.Reservoir) reservoirs (Coolant_Line attribute) residual_altitude() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle), [1] residual_total_forces() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Angle), [1] Residuals (class in RCAIDE.Framework.Mission.Common.Residuals) residuals() (Network method) resistance (DC_Generator attribute) (DC_Motor attribute) (PMSM_Generator attribute) (PMSM_Motor attribute) resize() (expanded_array method) Results (class in RCAIDE.Framework.Mission.Common.Results) reuse_stored_constant_speed_internal_combustion_engine_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.compute_constant_speed_internal_combustion_engine_performance) reuse_stored_data() (Constant_Speed_Internal_Combustion_Engine method) (Electric_Ducted_Fan method) (Electric_Rotor method) (Generic_Fuel_Cell_Stack method) (Internal_Combustion_Engine method) (Lithium_Ion_LFP method) (Lithium_Ion_NMC method) (Proton_Exchange_Membrane_Fuel_Cell method) (Turboelectric_Generator method) (Turbofan method) (Turbojet method) (Turboprop method) (Turboshaft method) reuse_stored_electric_ducted_fan_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.compute_electric_ducted_fan_performance) reuse_stored_electric_rotor_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.compute_electric_rotor_performance) reuse_stored_fuel_cell_data() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Larminie_Model.append_fuel_cell_conditions) (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.append_fuel_cell_conditions) reuse_stored_internal_combustion_engine_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.compute_internal_combustion_engine_performance) reuse_stored_lfp_cell_data() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.compute_lfp_cell_performance) reuse_stored_nmc_cell_data() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.compute_nmc_cell_performance) reuse_stored_turboelectric_generator_data() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboelectric_Generator.compute_turboelectric_generator_performance) reuse_stored_turbofan_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.compute_turbofan_performance) reuse_stored_turbojet_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.compute_turbojet_performance) reuse_stored_turboprop_data() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.compute_turboprop_performance) reuse_stored_turboshaft_data() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.compute_turboshaft_performance) RFMT_performance() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Rankine_Froude_Momentum_Theory.RFMT_performance) rho_A (Reformer attribute) rho_F (Reformer attribute) rho_S (Reformer attribute) RK4() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.heads_method) (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method) Rocket_LH2 (class in RCAIDE.Library.Attributes.Propellants.Rocket_LH2) Rocket_RP1 (class in RCAIDE.Library.Attributes.Propellants.Rocket_RP1) root_chord_percent (Segment attribute) rotate_points_with_quaternion() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.deflect_control_surface), [1] Rotor (class in RCAIDE.Library.Components.Powertrain.Converters.Rotor) rotor (Ducted_Fan attribute) (Electric_Rotor attribute) rotor_aerodynamic_analysis() (in module RCAIDE.Library.Methods.Performance.rotor_aerodynamic_analysis) rotor_radius (PMSM_Generator attribute) Rounded_Rectangle_Segment (class in RCAIDE.Library.Components.Fuselages.Segments.Rounded_Rectangle_Segment) Rudder (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Rudder) run_AVL_analysis() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.run_AVL_analysis) Run_Case (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Run_Case) Run_Case.Container (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Run_Case) run_dfdc_analysis() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.run_dfdc_analysis) run_objective_optimization() (Additive_Solver method), [1] run_rotor_cruise() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup) run_rotor_hover() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup) run_rotor_OEI() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup)

S

S_PZ (Combustor attribute) save() (in module RCAIDE.save) scale_const_bnds() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] scale_const_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] scale_input_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] scale_obj_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] scale_vals() (Additive_Solver method), [1] (Trust_Region_Optimization method), [1] SciPy_Problem() (in module RCAIDE.Framework.Optimization.Packages.scipy.scipy_setup), [1] SciPy_Solve() (in module RCAIDE.Framework.Optimization.Packages.scipy.scipy_setup), [1] sea_level_gravity (Earth attribute) sea_level_power (Engine attribute) secondary_cryogenic_flow (Cryogenic_Tank attribute) secondary_fuel_flow (Central_Fuel_Tank attribute) (Fuel_Tank attribute) (Wing_Fuel_Tank attribute) secondary_noise_component() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.secondary_noise_component), [1] Section (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing) Segment (class in RCAIDE.Framework.Mission.Segments.Segment) (class in RCAIDE.Library.Components.Fuselages.Segments.Segment) (class in RCAIDE.Library.Components.Nacelles.Segments.Segment) (class in RCAIDE.Library.Components.Wings.Segments.Segment) Segment.Container (class in RCAIDE.Framework.Mission.Segments.Segment) segment_centroid() (in module RCAIDE.Library.Methods.Geometry.Planform.wing_segmented_planform) Segment_Container (class in RCAIDE.Library.Components.Fuselages.Segments.Segment) (class in RCAIDE.Library.Components.Nacelles.Segments.Segment) (class in RCAIDE.Library.Components.Wings.Main_Wing) (class in RCAIDE.Library.Components.Wings.Segments.Segment) segment_post_process() (in module RCAIDE.Library.Mission.Solver.converge) segment_properties() (in module RCAIDE.Library.Methods.Geometry.Planform.wing_segmented_planform) segments (All_Moving_Surface attribute) (Boom attribute) (Fuselage attribute) (Main_Wing attribute) (Stack_Nacelle attribute) (Wing attribute) Sequential_Segments (class in RCAIDE.Framework.Mission.Sequential_Segments) sequential_segments() (in module RCAIDE.Library.Mission.Common.Segments), [1] Sequential_Segments.Container (class in RCAIDE.Framework.Mission.Sequential_Segments) set_ellipsoid() (Geodesic_Calculate method), [1] set_optimized_parameters() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.set_optimized_parameters) set_rated_current_density() (in module RCAIDE.Library.Methods.Powertrain.Converters.Fuel_Cells.Proton_Exchange_Membrane.compute_fuel_cell_performance) set_residuals_and_unknowns() (in module RCAIDE.Library.Mission.Common.Pre_Process.set_residuals_and_unknowns) set_section_angles() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom), [1] (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] set_sources() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.write_vsp_mesh) Set_Speed_Set_Altitude (class in RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude) Set_Speed_Set_Altitude_AVL_Trimmed (class in RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_AVL_Trimmed) Set_Speed_Set_Altitude_No_Propulsion (class in RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Altitude_No_Propulsion) Set_Speed_Set_Throttle (class in RCAIDE.Framework.Mission.Segments.Single_Point.Set_Speed_Set_Throttle) set_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] Settings (class in RCAIDE.Framework.Analyses.Settings) setup_operating_conditions() (in module RCAIDE.Library.Methods.Powertrain.setup_operating_conditions) Side_Cabin (class in RCAIDE.Library.Components.Fuselages.Cabins.Side_Cabin) sign_duplicate (Aileron attribute) (All_Moving_Surface attribute) (Control_Surface attribute) (Elevator attribute) (Flap attribute) (Rudder attribute) (Slat attribute) (Stabilator attribute) (Vertical_Tail_All_Moving attribute) sincosd() (Math static method), [1] sincosde() (Math static method), [1] size_core() (in module RCAIDE.Library.Methods.Powertrain.Converters.Turboshaft.size_core) (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbofan.size_core) (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet.size_core) (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Turboprop.size_core) size_module_from_energy_and_power() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.size_module_from_energy_and_power) size_module_from_mass() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Common.size_module_from_mass) skip() (in module RCAIDE.Library.Methods.skip) slack_constraint_1() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator) (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor) slack_constraint_2() (in module RCAIDE.Library.Methods.Powertrain.Converters.Generator.design_optimal_generator) (in module RCAIDE.Library.Methods.Powertrain.Converters.Motor.design_optimal_motor) Slat (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Slat) sol_tolerance (Rotor attribute) Solid (class in RCAIDE.Library.Attributes.Materials.Solid) solve_velocity() (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude), [1] span (Control_Surface attribute) span_fraction_end (Control_Surface attribute) span_fraction_start (Control_Surface attribute) spans (Wing attribute) species_list (Butanol attribute) (Ethane attribute) (Ethanol attribute) specific_energy (Alcohol_Mixture attribute) (Alkane_Mixture attribute) (Aluminum_Air.cell attribute) (Aviation_Gasoline attribute) (Butanol attribute) (Cryogen attribute) (Ethane attribute) (Ethanol attribute) (Gaseous_Hydrogen attribute) (Jet_A attribute) (Jet_A1 attribute) (JP7 attribute) (Liquid_Hydrogen attribute), [1] (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Lithium_Air.cell attribute) (Lithium_Sulfur.cell attribute) (Methane attribute) (Propane attribute) (Propanol attribute) (Propellant attribute)

specific_fuel_consumption_reduction_factor (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) specific_heat (Liquid_Hydrogen attribute) (Polyetherimide attribute) specific_heat_capacity (Air attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Coolant attribute) (Cross_Flow_Heat_Exchanger attribute) (Glycol_Water attribute) specific_power (Aluminum_Air.cell attribute) (Lithium_Air.cell attribute) (Lithium_Sulfur.cell attribute) spectral_shape_function_A() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) spectral_shape_function_B() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) speed_constant (DC_Generator attribute) (DC_Motor attribute) (PMSM_Generator attribute) (PMSM_Motor attribute) SPL_arithmetic() (in module RCAIDE.Library.Methods.Noise.Common.decibel_arithmetic), [1] SPL_average() (in module RCAIDE.Library.Methods.Noise.Common.decibel_arithmetic), [1] Spoiler (class in RCAIDE.Library.Components.Wings.Control_Surfaces.Spoiler) spoiler_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.spoiler_drag) sq() (Math static method), [1] Stabilator (class in RCAIDE.Library.Components.Wings.Stabilator) Stability (class in RCAIDE.Framework.Analyses.Stability.Stability) stability() (in module RCAIDE.Library.Mission.Common.Pre_Process.stability) (in module RCAIDE.Library.Mission.Common.Update.stability) stack_height (Cross_Flow_Heat_Exchanger attribute) stack_length (Cross_Flow_Heat_Exchanger attribute) Stack_Nacelle (class in RCAIDE.Library.Components.Nacelles.Stack_Nacelle) stack_width (Cross_Flow_Heat_Exchanger attribute) stall_line() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) stall_maneuver_speeds() (in module RCAIDE.Library.Methods.Performance.generate_V_n_diagram) STANDARD (Geodesic attribute), [1] (GeodesicCapability attribute), [1] State (class in RCAIDE.Framework.Mission.Common.State) State.Container (class in RCAIDE.Framework.Mission.Common.State) stator (Ducted_Fan attribute) stator_inner_diameter (PMSM_Motor attribute) stator_outer_diameter (PMSM_Motor attribute) Steam (class in RCAIDE.Library.Attributes.Gases.Steam) Steel (class in RCAIDE.Library.Attributes.Materials.Steel) stoichiometric_fuel_to_air (JP7 attribute) (Liquid_Hydrogen attribute) store_diff() (Container method) (Diffed_Data method) (Diffed_Data.Container method) strip_cumsum() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.VLM) strut_length (Landing_Gear attribute) (Main_Landing_Gear attribute) (Nose_Landing_Gear attribute) subsonic() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_wing_induced_velocity) sum() (Math static method), [1] sum_moment() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.mass_and_intertia_functions), [1] sum_moment_of_inertia() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.mass_and_intertia_functions), [1] Super_Ellipse_Segment (class in RCAIDE.Library.Components.Fuselages.Segments.Super_Ellipse_Segment) supersonic() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_wing_induced_velocity) supersonic_in_plane() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.compute_wing_induced_velocity) Supersonic_Nozzle (class in RCAIDE.Library.Components.Powertrain.Converters.Supersonic_Nozzle) supersonic_wave_drag_volume_raymer() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.supersonic_wave_drag_volume_raymer) supersonic_wave_drag_volume_sears_haack() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.supersonic_wave_drag_volume_sears_haack) surface_area (Reservoir attribute) surrogate_species_list (Butanol attribute) (Ethane attribute) (Ethanol attribute) sweep_distribution (Rotor attribute) sweeps (Segment attribute) (Wing attribute) symbolic (Wing attribute) symmetric (Vertical_Tail attribute) (Wing attribute) System (class in RCAIDE.Library.Components.Powertrain.Systems.System)

T

T0() (in module RCAIDE.Framework.Core.Utilities), [1] T1() (in module RCAIDE.Framework.Core.Utilities), [1] T2() (in module RCAIDE.Framework.Core.Utilities), [1] t_f (Cross_Flow_Heat_Exchanger attribute) t_tail (Wing attribute) t_w (Cross_Flow_Heat_Exchanger attribute) tag (Aileron attribute) (Air attribute) (Air_Cooled attribute) (Airfoil attribute) (Alcohol_Mixture attribute) (Alkane_Mixture attribute) (All_Moving_Surface attribute) (Aluminum_Air attribute) (Atmosphere attribute) (Aviation_Gasoline attribute) (Avionics attribute) (Biconvex_Airfoil attribute) (Blended_Wing_Body_Fuselage attribute) (Body_of_Revolution_Nacelle attribute) (Boom attribute) (Butanol attribute) (Central_Fuel_Tank attribute) (Circle_Segment attribute) (CO2 attribute) (Combustor attribute) (Component attribute) (Compression_Nozzle attribute) (Compressor attribute) (Config attribute) (Constant_Speed_Internal_Combustion_Engine attribute) (Control_Surface attribute) (Coolant attribute) (Coolant_Line attribute) (Cross_Flow_Heat_Exchanger attribute) (Cryogen attribute) (Cryogenic_Tank attribute) (DC_Generator attribute) (DC_Motor attribute) (Ducted_Fan attribute) (Earth attribute) (Electric attribute) (Electric_Ducted_Fan attribute) (Electric_Rotor attribute) (Electrical_Bus attribute) (Electronic_Speed_Controller attribute) (Elevator attribute) (Ellipse_Segment attribute) (Engine attribute) (Ethane attribute) (Ethanol attribute) (Expansion_Nozzle attribute) (Fan attribute), [1] (Flap attribute) (Fuel attribute) (Fuel_Cell attribute) (Fuel_Line attribute) (Fuel_Selector attribute) (Fuel_Tank attribute) (Fuselage attribute) (Gas attribute) (Gaseous_Hydrogen attribute) (Glycol_Water attribute) (Horizontal_Tail attribute) (Hybrid attribute) (Internal_Combustion_Engine attribute) (Jet_A attribute) (Jet_A1 attribute) (JP7 attribute) (Landing_Gear attribute) (Lift_Rotor attribute) (Liquid_Hydrogen attribute), [1] (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Lithium_Ion_LFP attribute) (Lithium_Ion_NMC attribute) (Main_Landing_Gear attribute) (Main_Wing attribute) (Methane attribute) (NACA_4_Series_Airfoil attribute) (Nacelle attribute) (Network attribute), [1] (Nose_Landing_Gear attribute) (Payload attribute) (PMSM_Generator attribute) (PMSM_Motor attribute) (Prop_Rotor attribute) (Propane attribute) (Propanol attribute) (Propellant attribute) (Propeller attribute) (Propulsor attribute) (Pump attribute) (Ram attribute) (Reformer attribute) (Reservoir attribute) (Rocket_LH2 attribute) (Rocket_RP1 attribute) (Rotor attribute) (Rounded_Rectangle_Segment attribute) (Rudder attribute) (Segment attribute), [1], [2] (Slat attribute) (Spoiler attribute) (Stabilator attribute) (Stack_Nacelle attribute) (Steam attribute) (Super_Ellipse_Segment attribute) (Supersonic_Nozzle attribute) (System attribute) (Tube_Fuselage attribute) (Turbine attribute) (Turboelectric_Generator attribute) (Turbofan attribute) (Turbojet attribute) (Turboprop attribute) (Turboshaft attribute) (Vertical_Tail attribute) (Vertical_Tail_All_Moving attribute) (Wing attribute) (Wing_Fuel_Tank attribute)

tail_curvature (Fuselage attribute) Takeoff (class in RCAIDE.Framework.Mission.Segments.Ground.Takeoff) taper (Segment attribute) (Wing attribute) Taylor_number (PMSM_Motor attribute) TBL_TE_broadband_noise() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TBL_TE_broadband_noise) temperature (Gaseous_Hydrogen attribute) temperature_range (CrossLinked_Polyethylene attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) temperatures (Coolant attribute) (Cryogen attribute) (Jet_A1 attribute) (JP7 attribute) (Liquid_Hydrogen attribute), [1] (Propellant attribute) thermal_conductivity (Aluminum attribute) (Aluminum_Alloy attribute) (Coolant attribute) (Cross_Flow_Heat_Exchanger attribute) (CrossLinked_Polyethylene attribute) (Glycol_Water attribute) (Perfluoroalkoxy attribute) (PMSM_Motor attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) thermal_conductivity() (Copper method) thermal_conductivity_fluid (PMSM_Motor attribute) theta (Compression_Nozzle attribute) (Reformer attribute) thickness (Reservoir attribute) thickness_to_chord (Rotor attribute) (Segment attribute) (Wing attribute) thrust() (in module RCAIDE.Library.Mission.Common.Update.thrust) thwaites_method() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.thwaites_method) time() (in module RCAIDE.Library.Mission.Common.Initialize.time) tiny_ (Geodesic attribute), [1] TIP_broadband_noise() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.TIP_broadband_noise) tip_radius (Ducted_Fan attribute) (Rotor attribute) tire_diameter (Landing_Gear attribute) (Main_Landing_Gear attribute) (Nose_Landing_Gear attribute) Titanium (class in RCAIDE.Library.Attributes.Materials.Titanium) tol0_ (Geodesic attribute), [1] tol1_ (Geodesic attribute), [1] tol2_ (Geodesic attribute), [1] tolb_ (Geodesic attribute), [1] total_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.total_drag) total_length (Wing attribute) trailing_edge_flap_noise() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe.trailing_edge_flap_noise) train_AVL_surrogates() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.train_AVL_surrogates) train_CRN_EI_surrogates() (in module RCAIDE.Library.Methods.Emissions.Chemical_Reactor_Network_Method.train_CRN_EI_surrogates) train_model() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.train_VLM_surrogates) train_trasonic_model() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.train_VLM_surrogates) train_VLM_surrogates() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.train_VLM_surrogates) transition_x_lower (Wing attribute) transition_x_upper (Wing attribute) translate() (Nexus method) translate_avl_body() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures), [1] translate_avl_wing() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures), [1] translate_conditions_to_cases() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.translate_data), [1] translate_conditions_to_dfdc_cases() (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.translate_conditions_to_dfdc_cases) translate_results_to_conditions() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.translate_data), [1] transonic_drag_function() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.compressibility_drag) TRMM_Solve() (in module RCAIDE.Framework.Optimization.Packages.trmm.TRMM_setup), [1] truncate_colormap() (in module RCAIDE.Library.Methods.Performance.compute_noise_certification_data), [1] (in module RCAIDE.Library.Plots.Noise.plot_2D_noise_contour) Trust_Region (class in RCAIDE.Framework.Optimization.Packages.trmm.Trust_Region), [1] Trust_Region_Optimization (class in RCAIDE.Framework.Optimization.Packages.trmm.Trust_Region_Optimization), [1] Tube_Fuselage (class in RCAIDE.Library.Components.Fuselages.Tube_Fuselage) Turbine (class in RCAIDE.Library.Components.Powertrain.Converters.Turbine) turbine (Turboprop attribute) turbine_inlet_temperature (Combustor attribute) Turboelectric_Generator (class in RCAIDE.Library.Components.Powertrain.Converters.Turboelectric_Generator) Turbofan (class in RCAIDE.Library.Components.Powertrain.Propulsors.Turbofan) turbofan_engine_noise() (in module RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.turbofan_engine_noise) Turbojet (class in RCAIDE.Library.Components.Powertrain.Propulsors.Turbojet) Turboprop (class in RCAIDE.Library.Components.Powertrain.Propulsors.Turboprop) Turboshaft (class in RCAIDE.Library.Components.Powertrain.Converters.Turboshaft) turboshaft (Turboelectric_Generator attribute) twist (Segment attribute) twist_distribution (Rotor attribute) twists (Wing attribute) typestring() (Data method) (DataOrdered method)

U

ultimate_bearing_strength (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute) ultimate_shear_strength (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute) ultimate_tensile_strength (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute) unflatten_matrix() (in module RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor.broadband_noise) Unidirectional_Carbon_Fiber (class in RCAIDE.Library.Attributes.Materials.Unidirectional_Carbon_Fiber) units (Landing_Gear attribute) (Main_Landing_Gear attribute) (Nose_Landing_Gear attribute) Unknowns (class in RCAIDE.Framework.Mission.Common.Unknowns) unknowns() (in module RCAIDE.Library.Mission.Common.Unpack_Unknowns.energy), [1] unpack_array() (Data method) unpack_body_angle() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed), [1] unpack_constraints_slsqp() (Additive_Solver method), [1] (Trust_Region_Optimization method), [1]

unpack_electric_ducted_fan_unknowns() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Ducted_Fan.unpack_electric_ducted_fan_unknowns) unpack_electric_rotor_unknowns() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Electric_Rotor.unpack_electric_rotor_unknowns) unpack_inputs() (Nexus method) unpack_internal_combustion_engine_unknowns() (in module RCAIDE.Library.Methods.Powertrain.Propulsors.Internal_Combustion_Engine.unpack_internal_combustion_engine_unknowns) unpack_propulsor_unknowns() (Constant_Speed_Internal_Combustion_Engine method) (Electric_Ducted_Fan method) (Electric_Rotor method) (Internal_Combustion_Engine method) (Turbofan method) (Turbojet method) (Turboprop method) (Turboshaft method) unpack_unknowns() (in module RCAIDE.Library.Mission.Segments.Cruise.Constant_Throttle_Constant_Altitude), [1] (in module RCAIDE.Library.Mission.Segments.Single_Point.Set_Speed_Set_Throttle), [1] (Network method) unscale_const_values() (in module RCAIDE.Framework.Optimization.Common.helper_functions), [1] Untrimmed (class in RCAIDE.Framework.Mission.Segments.Untrimmed.Untrimmed) update() (DataOrdered method) update_battery_age() (Lithium_Ion_LFP method) (Lithium_Ion_NMC method) update_differentials() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Dynamic_Pressure_Constant_Angle), [1] (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Mach_Constant_Angle), [1] update_differentials_altitude() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed), [1] update_lfp_cell_age() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_LFP.update_lfp_cell_age) update_nmc_cell_age() (in module RCAIDE.Library.Methods.Powertrain.Sources.Batteries.Lithium_Ion_NMC.update_nmc_cell_age) update_origin() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.import_vsp_vehicle) update_seat_map_layout_using_cabin_taper() (in module RCAIDE.Library.Methods.Geometry.LOPA.LOPA_functions), [1] update_tr_size() (Trust_Region_Optimization method), [1] update_velocity_vector_from_wind_angle() (in module RCAIDE.Library.Mission.Segments.Climb.Constant_Throttle_Constant_Speed), [1] updated_blade_geometry() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Design.procedure_setup) upper_bound (Aluminum_Air.cell.ragone attribute) (Lithium_Sulfur.cell.ragone attribute) US_Standard_1976 (class in RCAIDE.Framework.Analyses.Atmospheric.US_Standard_1976) (class in RCAIDE.Library.Attributes.Atmospheres.Earth.US_Standard_1976) use_2d_analysis (Lift_Rotor attribute) (Prop_Rotor attribute) (Propeller attribute) (Rotor attribute) use_constant_hinge_fraction (All_Moving_Surface attribute) use_high_fidelity_kinetics_model (Butanol attribute) (Ethane attribute) (Ethanol attribute) (Jet_A attribute) (Liquid_Natural_Gas attribute) (Liquid_Petroleum_Gas attribute) (Methane attribute) (Propane attribute) (Propanol attribute)

V

V_cat (Reformer attribute) va_vt() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] values() (DataOrdered method) vaporization_coefficients (Liquid_Hydrogen attribute) vaporization_enthalpy (Liquid_Hydrogen attribute) vec_to_duct_body() (Ducted_Fan method) vec_to_prop_body() (Rotor method) vec_to_vel() (Ducted_Fan method) (Nacelle method) (Rotor method) Vehicle (class in RCAIDE.Framework.Analyses.Vehicle) (class in RCAIDE.Vehicle) Vehicle_Mass_Container (class in RCAIDE.Vehicle) Vehicle_Mass_Properties (class in RCAIDE.Vehicle) velocity_distribution() (in module RCAIDE.Library.Methods.Aerodynamics.Airfoil_Panel_Method.velocity_distribution) velocity_of_fluid (PMSM_Motor attribute) vertical (Vertical_Tail attribute) (Wing attribute)

Vertical_Tail (class in RCAIDE.Library.Components.Wings.Vertical_Tail) Vertical_Tail_All_Moving (class in RCAIDE.Library.Components.Wings.Vertical_Tail_All_Moving) vertical_tail_planform() (in module RCAIDE.Library.Methods.Geometry.Planform.vertical_tail_planform) vertical_tail_planform_raymer() (in module RCAIDE.Library.Methods.Geometry.Planform.vertical_tail_planform_raymer) VLM() (in module RCAIDE.Library.Methods.Aerodynamics.Vortex_Lattice_Method.VLM) voltage (Electrical_Bus attribute) volume (Mass_Properties attribute) (Reservoir attribute) volume_flow_rate_of_fluid (PMSM_Motor attribute) Volume_Fraction() (in module RCAIDE.Library.Methods.Mass_Properties.Moment_of_Inertia.compute_fuselage_moment_of_inertia) volume_packaging_factor (Generic_Battery_Module attribute) Vortex_Lattice_Method (class in RCAIDE.Framework.Analyses.Aerodynamics.Vortex_Lattice_Method) (class in RCAIDE.Framework.Analyses.Stability.Vortex_Lattice_Method) vortex_lift (Wing attribute) vsp_data (Boom attribute) (Fuselage attribute) vtk_airfoil_points (Rotor attribute)

W

wake_convergence() (in module RCAIDE.Library.Methods.Powertrain.Converters.Rotor.Performance.Blade_Element_Momentum_Theory_Helmholtz_Wake.wake_model), [1] wall_conductivity (Cross_Flow_Heat_Exchanger attribute) water_mass_gain_factor (Aluminum_Air.cell attribute) wave_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.wave_drag) wave_drag_lift() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.wave_drag_lift) wavy_channel_design_problem_setup() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.design_wavy_channel) wavy_channel_geometry_setup() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_geometry_setup) wavy_channel_rating_model() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_rating_model) wavy_channel_sizing_setup() (in module RCAIDE.Library.Methods.Thermal_Management.Batteries.Liquid_Cooled_Wavy_Channel.wavy_channel_sizing_setup) Weights (class in RCAIDE.Framework.Analyses.Weights.Weights) weights() (in module RCAIDE.Library.Mission.Common.Initialize.weights) (in module RCAIDE.Library.Mission.Common.Update.weights) WGS84 (Geodesic attribute), [1] WGS84_a (Constants attribute), [1] WGS84_f (Constants attribute), [1] wheels (Landing_Gear attribute) (Main_Landing_Gear attribute) (Nose_Landing_Gear attribute) width (Boom attribute) (Central_Fuel_Tank attribute) (Circle_Segment attribute) (Ellipse_Segment attribute) (Fuselage attribute) (Generic_Battery_Module attribute) (Reservoir attribute) (Rounded_Rectangle_Segment attribute) (Segment attribute), [1] (Super_Ellipse_Segment attribute) (Wing_Fuel_Tank attribute)

width_of_duct (PMSM_Motor attribute) winding_factor (PMSM_Motor attribute) windmilling_drag() (in module RCAIDE.Library.Methods.Aerodynamics.Common.Drag.windmilling_drag) Wing (class in RCAIDE.Library.Components.Wings.Wing) (class in RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing) Wing.Container (class in RCAIDE.Library.Components.Wings.Wing) Wing_Fuel_Tank (class in RCAIDE.Library.Components.Powertrain.Sources.Fuel_Tanks.Wing_Fuel_Tank) wing_fuel_volume() (in module RCAIDE.Library.Methods.Geometry.Planform.wing_fuel_volume) wing_mounted (Propulsor attribute) wing_planform() (in module RCAIDE.Library.Methods.Geometry.Planform.wing_planform) wing_segmented_planform() (in module RCAIDE.Library.Methods.Geometry.Planform.wing_segmented_planform) wing_weight_constants_FLOPS() (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.FLOPS.compute_wing_weight) (in module RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport.FLOPS.compute_wing_weight) working_fluid (Ram attribute) write_avl_airfoil_file() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_avl_airfoil_file) write_fuselage_conformal_fuel_tank() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] write_geometry() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_geometry) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_geometry) write_input_deck() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_input_deck) (in module RCAIDE.Library.Methods.Powertrain.Converters.Ducted_Fan.Performance.Blade_Element_Momentum_Theory.write_input_deck) write_mass_file() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_mass_file) write_run_cases() (in module RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.write_run_cases) write_vsp_boom() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_boom), [1] write_vsp_control_surface() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing), [1] write_vsp_fuselage() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_fuselage), [1] write_vsp_mesh() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.write_vsp_mesh) write_vsp_nacelle() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_nacelle), [1] write_vsp_rotor_bem() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_rotor), [1] write_vsp_wing() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing), [1] write_wing_conformal_fuel_tank() (in module RCAIDE.Framework.External_Interfaces.OpenVSP.vsp_wing), [1]

X

x_C (Reformer attribute) x_H (Reformer attribute)

x_rotation (Boom attribute) (Fuselage attribute) xthresh_ (Geodesic attribute), [1]

Y

y_CO (Reformer attribute) y_H2 (Reformer attribute) y_rotation (Boom attribute) (Fuselage attribute) yield_bearing_strength (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute) yield_shear_strength (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute)

yield_tensile_strength (Acrylic attribute) (Aluminum attribute) (Aluminum_Alloy attribute) (Bidirectional_Carbon_Fiber attribute) (Carbon_Fiber_Honeycomb attribute) (CrossLinked_Polyethylene attribute) (Epoxy attribute) (Magnesium attribute) (Nickel attribute) (Paint attribute) (Perfluoroalkoxy attribute) (Polyimide attribute) (Polytetrafluoroethylene attribute) (Solid attribute) (Steel attribute) (Titanium attribute) (Unidirectional_Carbon_Fiber attribute)

Z

z_rotation (Boom attribute) (Fuselage attribute)