Module veloren_common::comp::fluid_dynamics
source · Structs§
Enums§
- Fluid medium in which the entity exists
Functions§
- Geometric angle of attack
- Total lift coefficient for a finite wing of symmetric aerofoil shape and elliptical pressure distribution.
- 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