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SaveAeroCoefficients

Categories: Aerodynamics, Results, Plot

State: ✔️

SaveAeroCoefficients module allows to plot aerodynamic coefficients calculated by the different modules of CEASIOMpy.

Inputs

SaveAeroCoefficients only takes as input a CPACS file. It must contain at least one aeromap to plot.

Analyses

Nothing is calculated by this module, it just plots the aerodynamic coefficients with Matplotlib.

Outputs

SaveAeroCoefficients only open a new window to show the coefficients, you can then save manually.

Installation or requirements

SaveAeroCoefficients is a native CEASIOMpy module, hence it is available and installed by default. To run it, you just have to be sure that you are in the CEASIOMpy Conda environment.

Limitations

For now SaveAeroCoefficients do not save the figures automatically, you must save them manually.