buffalo_wings.wing.EvaluatedStation

class buffalo_wings.wing.EvaluatedStation(panel_id, eta, y, x_ref, z_ref, chord, twist_rad)[source]

Bases: object

Evaluated panel properties at a span station.

Parameters:

panel_id (str)
eta (buffalo_wings.type_aliases.FloatScalar)
y (buffalo_wings.type_aliases.FloatScalar)
x_ref (buffalo_wings.type_aliases.FloatScalar)
z_ref (buffalo_wings.type_aliases.FloatScalar)
chord (buffalo_wings.type_aliases.FloatScalar)
twist_rad (buffalo_wings.type_aliases.FloatScalar)

panel_id

Identifier of the panel evaluated at this station.

Type:: str

eta

Normalized spanwise coordinate used for evaluation.

Type:: buffalo_wings.type_aliases.FloatScalar

Spanwise position in the wing reference frame.

Type:: buffalo_wings.type_aliases.FloatScalar

x_ref

Reference-axis x-position at the span station.

Type:: buffalo_wings.type_aliases.FloatScalar

z_ref

Reference-axis z-position at the span station.

Type:: buffalo_wings.type_aliases.FloatScalar

chord

Local chord length at the span station.

Type:: buffalo_wings.type_aliases.FloatScalar

twist_rad

Local twist angle in radians.

Type:: buffalo_wings.type_aliases.FloatScalar

__init__(panel_id, eta, y, x_ref, z_ref, chord, twist_rad)

Parameters:

panel_id (str)
eta (buffalo_wings.type_aliases.FloatScalar)
y (buffalo_wings.type_aliases.FloatScalar)
x_ref (buffalo_wings.type_aliases.FloatScalar)
z_ref (buffalo_wings.type_aliases.FloatScalar)
chord (buffalo_wings.type_aliases.FloatScalar)
twist_rad (buffalo_wings.type_aliases.FloatScalar)

Return type:

None

Methods

__init__(panel_id, eta, y, x_ref, z_ref, ...)

Attributes

`panel_id`
`eta`
`y`
`x_ref`
`z_ref`
`chord`
`twist_rad`