RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.General_Aviation.Raymer

Raymer

RCAIDE Package Setup

Modules

compute_fuselage_weight(fuselage, vehicle, l_ht)	Calculate the weight of a fuselage for a GA aircraft
compute_horizontal_tail_weight(wing, vehicle)	Calculate the weight of the horizontal tail for a General Aviation-type aircraft
compute_landing_gear_weight(landing_weight, ...)	Calculate the weight of the landing gear
compute_main_wing_weight(wing, vehicle, m_fuel)	Calculate the weight of the main wing of an aircraft
compute_operating_empty_weight(vehicle[, ...])	output = RCAIDE.Methods.Weights.Correlations.Tube_Wing.empty(engine,wing,aircraft,fuselage,horizontal,vertical)
compute_payload_weight(vehicle[, ...])	Calculate the weight of the payload and the resulting fuel mass
compute_propulsion_system_weight(network)
compute_systems_weight(vehicle, V_fuel, ...)	output = RCAIDE.Methods.Weights.Correlations.General_Avation.systems(num_seats, ctrl_type, S_h, S_v, S_gross_w, ac_type) Calculate the weight of the different engine systems on the aircraft
compute_vertical_tail_weight(wing, vehicle)	Calculate the weight of the vertical fin of an aircraft without the weight of the rudder and then calculate the weight of the rudder