buffalo_wings.airfoil.CstSurfaceSpec

class buffalo_wings.airfoil.CstSurfaceSpec(n1, n2, a=<factory>)

Bases: object

CST coefficient set for one airfoil surface.

Parameters:

• n1 (float)

• n2 (float)

• a (list[float])

n1

Leading-edge class function exponent.

Type:

float

n2

Trailing-edge class function exponent.

Type:

float

a

Shape-function coefficients for the surface polynomial basis.

Type:

list[float], optional

__init__(n1, n2, a=<factory>)

Parameters:

• n1 (float)

• n2 (float)

• a (list[float])

Return type:

None

Methods

__init__(n1, n2[, a])

Attributes

n1
n2
a