-
-
Notifications
You must be signed in to change notification settings - Fork 251
ENH: Variation of CL with Mach (nose and tail) #133
Copy link
Copy link
Labels
AerodynamicsAny problem to be worked on top of RocketPy's AerodynamicAny problem to be worked on top of RocketPy's AerodynamicEnhancementNew feature or request, including adjustments in current codesNew feature or request, including adjustments in current codes
Milestone
Metadata
Metadata
Assignees
Labels
AerodynamicsAny problem to be worked on top of RocketPy's AerodynamicAny problem to be worked on top of RocketPy's AerodynamicEnhancementNew feature or request, including adjustments in current codesNew feature or request, including adjustments in current codes
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