RCAIDE.Library.Methods.Aerodynamics.Common.Drag

Drag

RCAIDE Package Setup

Modules

asymmetry_drag(state, geometry[, ...])	Computes asymmetry drag due to engine failure
compressibility_drag(state, settings, geometry)	Computes compressibility drag for full aircraft including volume drag
compressible_mixed_flat_plate(Re, Ma, Tc, xt)	Computes the coefficient of friction for a flat plate given the input parameters.
compressible_turbulent_flat_plate(Re, Ma, Tc)	Computes the coefficient of friction for a flat plate given the input parameters.
cooling_drag(state, settings, geometry)	Computes the cooling drag based on the results of the Heat Exchanger operation
drag_divergence(Mach, geometry, Cl)	Use drag divergence Mach number to determine drag for subsonic speeds
estimate_2ndseg_lift_drag_ratio(state, ...)	Estimates the 2nd segment climb lift to drag ratio (all engine operating)
induced_drag(state, settings, geometry)	Determines induced drag for the full aircraft
lift_wave_drag(conditions, wing, Sref)	Determine lift wave drag for supersonic speeds.
miscellaneous_drag(state, settings, geometry)	Computes the miscellaneous drag associated with an aircraft
parasite_drag_fuselage(state, settings, fuselage)	Computes the parasite drag due the a fuselage (or boom)
parasite_drag_nacelle(state, settings, geometry)	Computes the parasite drag due to the nacelle
parasite_drag_pylon(state, settings, geometry)	Computes the parasite drag due to pylons as a proportion of the network
parasite_drag_wing(state, settings, geometry)	Computes the parasite drag due to wings
parasite_total(state, settings, geometry)	Sums up the parasite drags from all compoments
spoiler_drag(state, settings, geometry)	Updates the aerodynamic performance of an aircraft given the influence of deflected spoilers
supersonic_wave_drag_volume_raymer(vehicle, ...)	Computes the volume drag
supersonic_wave_drag_volume_sears_haack(...)	Computes the volume drag
total_drag(state, settings, geometry)	Computes the total drag of an aircraft.
wave_drag(conditions, wing)	Computes wave drag due to lift
wave_drag_lift(conditions, configuration, wing)	Computes wave drag due to lift
windmilling_drag(geometry, state)	Computes windmilling drag for turbofan engines