buffalo_wings.airfoil.PointsAirfoilSpec

class buffalo_wings.airfoil.PointsAirfoilSpec(type='points', format='surface_curve', leading_edge=None, points=<factory>, upper=<factory>, lower=<factory>)[source]

Bases: object

Airfoil schema defined directly from inline point coordinates.

Attributes

`type`	Schema discriminator for an inline point-defined airfoil.
`format`	Point-layout convention used by the inline coordinate payload.
`leading_edge`	Leading-edge split index for `surface_curve` point ordering.
`points`	Single ordered surface walk when `format == "surface_curve"`.
`upper`	Upper-surface points when `format == "upper_lower"`.
`lower`	Lower-surface points when `format == "upper_lower"`.

type: Literal['points']: Schema discriminator for an inline point-defined airfoil.

format: Literal['surface_curve', 'upper_lower']: Point-layout convention used by the inline coordinate payload.

leading_edge: int | None: Leading-edge split index for surface_curve point ordering.

points: list[tuple[float, float]]: Single ordered surface walk when format == "surface_curve".

upper: list[tuple[float, float]]: Upper-surface points when format == "upper_lower".

lower: list[tuple[float, float]]: Lower-surface points when format == "upper_lower".