buffalo_wings.airfoil.CstAirfoilSpec

class buffalo_wings.airfoil.CstAirfoilSpec(type='cst', trailing_edge_thickness=0.0, upper=<factory>, lower=<factory>)[source]

Bases: object

Schema definition for a CST airfoil.

Attributes

`type`	Schema discriminator for a CST airfoil.
`trailing_edge_thickness`	Explicit trailing-edge gap as a fraction of chord.
`upper`	CST coefficients for the upper surface.
`lower`	CST coefficients for the lower surface.

trailing_edge_thickness: float: Explicit trailing-edge gap as a fraction of chord.