buffalo_wings.airfoil.Naca16AirfoilParamsSpec

class buffalo_wings.airfoil.Naca16AirfoilParamsSpec(ideal_lift_coefficient=0.0, max_thickness=0.0)[source]

Bases: object

Explicit parameter definition for a NACA 16-series airfoil.

Attributes

`ideal_lift_coefficient`	Ideal lift coefficient encoded by the designation family.
`max_thickness`	Maximum thickness as a fraction of chord.

ideal_lift_coefficient: FloatScalar: Ideal lift coefficient encoded by the designation family.