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You have to simulate the flow around a rocket at AoA 0, Mach 0.35, altitude 0 slm, ISA atmosphere - Copy
by slilbaekslilbaek
You have to simulate the flow around a rocket at AoA 0, Mach 0.35, altitude 0 slm, ISA atmosphere - Copy
gbeghetto created this project
over 5 years ago
kaddai_boateng copied this project
over 2 years ago