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ENH: Variation of CL with Mach (nose and tail) #133

@Gui-FernandesBR

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@Gui-FernandesBR

Currently we have calculation of Lif Coefficient in function of Mach Number for our fins, but in the future will be important having the same approach for the nosecone and tail

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AerodynamicsAny problem to be worked on top of RocketPy's AerodynamicEnhancementNew feature or request, including adjustments in current codes

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