Structs

Enums

Functions

  • Geometric angle of attack
  • Total lift coefficient for a finite wing of symmetric aerofoil shape and elliptical pressure distribution.
  • lift_slope 🔒
    The change in lift over change in angle of attack¹. Multiplying by angle of attack gives the lift coefficient (for a finite wing, not aerofoil). Aspect ratio is the ratio of total wing span squared over planform area.
  • The zero-lift profile drag coefficient is the parasite drag on the wings at the angle of attack which generates no lift