buffalo_wings.wing.PanelSpec

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

Bases: object

Parametric definition of a single spanwise wing panel.

Parameters:

Unique panel identifier within the wing definition.

eta_range

Inclusive spanwise parameter range covered by the panel.

ref_line

Reference-axis position distributions for the panel.

chord

Spanwise chord distribution over eta_range.

twist

Spanwise twist distribution over eta_range.

airfoil

Airfoil definition or blend applied across the panel.

nurbs

Optional panel-local NURBS construction overrides.

mesh

Optional export mesh sampling overrides for the panel.

__init__(id, eta_range, ref_line, chord, twist, airfoil, nurbs=None, mesh=None)

Parameters:

Return type:

None

Methods

__init__(id, eta_range, ref_line, chord, ...)

Attributes