buffalo_wings.airfoil.CstSurfaceSpec

class buffalo_wings.airfoil.CstSurfaceSpec(n1=0.5, n2=1.0, a=<factory>)[source]

Bases: object

CST coefficient set for one airfoil surface.

Attributes

n1

Leading-edge class-function exponent.

n2

Trailing-edge class-function exponent.

a

Bernstein polynomial coefficients for the surface shape.

n1: float

Leading-edge class-function exponent.

n2: float

Trailing-edge class-function exponent.

a: list[float]

Bernstein polynomial coefficients for the surface shape.