buffalo_wings.airfoil.Naca6ACamberComponentSpec

class buffalo_wings.airfoil.Naca6ACamberComponentSpec(ideal_lift_coefficient=0.0)[source]

Bases: object

One additive mean-line component for a NACA 6A-series airfoil.

Attributes

ideal_lift_coefficient

Ideal lift coefficient for this additive mean-line component.
ideal_lift_coefficient: FloatScalar

Ideal lift coefficient for this additive mean-line component.