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Dassault Mirage 2000 - Aerodynamics - Copy - Copy
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2 Geometries
3 Meshes
2 Simulation setups
2 Results
2 Geometries 3 Meshes 2 Simulation setups 2 ResultsAbout this project
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 - Copy - Copy
