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rocket_1 - Copy

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kaddai_boateng
kaddai_boateng
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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

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Project History

  • gbeghetto

    gbeghetto created this project

  • kaddai_boateng

    kaddai_boateng copied this project