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You have to simulate the flow around a rocket (.STEP file attached) at AoA equal 0, Mach 0.35, Altitude 0 s.l.m., ISA atmosphere.
by slilbaekslilbaek
pionao created this project
almost 6 years ago
You have to simulate the flow around a rocket (.STEP file attached) at AoA equal 0, Mach 0.35, Altitude 0 s.l.m., ISA atmosphere.