RCAIDE.Library.Methods.Aerodynamics.Common.Lift.compute_slat_lift

compute_slat_lift

compute_slat_lift(slat_angle, sweep_angle)

Computes the increase in lift due to slats

Assumptions: None

Source: adg.stanford.edu (Stanford AA241 A/B Course Notes)

Inputs: slat_angle [radians] sweep_angle [radians]

Outputs: dcl_slat [Unitless]

Properties Used: N/A