RCAIDE.Library.Methods.Aerodynamics.Common.Lift

Lift

RCAIDE Package Setup

Modules

BET_calculations
compute_flap_lift(t_c, flap_type, ...)	Computes the increase of lift due to trailing edge flap deployment
compute_max_lift_coeff(state, settings, geometry)	Computes the maximum lift coefficient associated with an aircraft high lift system
compute_slat_lift(slat_angle, sweep_angle)	Computes the increase in lift due to slats
fuselage_correction(state, settings, geometry)	Corrects aircraft lift based on fuselage effects