ENH: Variation of CL with Mach (nose and tail) #133
Labels
Aerodynamics
Any problem to be worked on top of RocketPy's Aerodynamic
Enhancement
New feature or request, including adjustments in current codes
Milestone
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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