Fins Plots Class#

class rocketpy.plots.aero_surface_plots._FinsPlots[source]#

Abstract class that contains all fin plots. This class inherits from the _AeroSurfacePlots class.

__init__(fin_set)[source]#

Initialize the class

Parameters:

fin_set (rocketpy.AeroSurface.fin_set) – fin_set object to be plotted

Return type:

None

airfoil()[source]#

Plots the airfoil information when the fin has an airfoil shape. If the fin does not have an airfoil shape, this method does nothing.

Return type:

None

roll()[source]#

Plots the roll parameters of the fin set.

Return type:

None

lift()[source]#

Plots the lift coefficient of the aero surface as a function of Mach and the angle of attack. A 3D plot is expected. See the rocketpy.Function class for more information on how this plot is made. Also, this method plots the lift coefficient considering a single fin and the lift coefficient considering all fins.

Return type:

None

all()[source]#

Plots all available fin plots.

Return type:

None