AeroSurface Abstract Class#

class rocketpy.AeroSurface[source]#

Abstract class used to define aerodynamic surfaces.

__init__(name)[source]#
abstract evaluate_center_of_pressure()[source]#

Evaluates the center of pressure of the aerodynamic surface in local coordinates.

Return type:

None

abstract evaluate_lift_coefficient()[source]#

Evaluates the lift coefficient curve of the aerodynamic surface.

Return type:

None

abstract evaluate_geometrical_parameters()[source]#

Evaluates the geometrical parameters of the aerodynamic surface.

Return type:

None

abstract info()[source]#

Prints and plots summarized information of the aerodynamic surface.

Return type:

None

abstract all_info()[source]#

Prints and plots all the available information of the aero surface.

Return type:

None