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.
- airfoil(*, filename=None)[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.
- Parameters:
filename (
str | None, optional) – The path the plot should be saved to. By default None, in which case the plot will be shown instead of saved.- Return type:
None
- roll(*, filename=None)[source]#
Plots the roll parameters of the fin set.
- Parameters:
filename (
str | None, optional) – The path the plot should be saved to. By default None, in which case the plot will be shown instead of saved.- Return type:
None
- lift(*, filename=None)[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.
- Parameters:
filename (
str | None, optional) – The path the plot should be saved to. By default None, in which case the plot will be shown instead of saved.- Return type:
None