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Dassault Mirage 2000 - Aerodynamics

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brototype
brototype
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Some compressible and incompressible simulations on Dassault Mirage 2000 - Delta Wing - jet. - High AoA flight: 15 degrees Angle of attack at 195 Kts (Landing configuration) flow visualization. - Supersonic Flight: mach 1.5 at 32.000 ft. Bowshock visualization. - Inlet flow visualization

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Project History

  • alfiosky4

    alfiosky4 created this project

  • brototype

    brototype copied this project