buffalo_wings.wing.PanelSpec

class buffalo_wings.wing.PanelSpec(id, eta_range, ref_line, chord, twist, airfoil, nurbs=None, mesh=None)

Bases: object

Parametric definition of a single spanwise wing panel.

Attributes

id	Unique panel identifier.
eta_range	Closed spanwise eta interval covered by the panel.
ref_line	Reference-line position distributions for the panel.
chord	Chord distribution over the panel span.
twist	Twist distribution over the panel span.
airfoil	Airfoil reference or blend assigned to the panel.
nurbs	Optional NURBS construction controls.
mesh	Optional mesh export controls.

id: str

Unique panel identifier.

eta_range: tuple[float, float]

Closed spanwise eta interval covered by the panel.

ref_line: RefLineSpec

Reference-line position distributions for the panel.

chord: DistributionSpec

Chord distribution over the panel span.

twist: DistributionSpec

Twist distribution over the panel span.

airfoil: AirfoilRefSpec

Airfoil reference or blend assigned to the panel.

nurbs: NurbsSpec | None

Optional NURBS construction controls.

mesh: MeshSpec | None

Optional mesh export controls.