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CFD Final Wings - selig
150 0
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8 Geometries 7 Meshes 5 Simulation setups 5 Results
About this project
Simulate drag and efficiency of prototype wing. Incompressible subsonic flow at 8m/s 'x' axis. - fuselage. Updated to fit the launcher spec. - Copy - Copy - Copy
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by Ali_ArafatAli_Arafat
Project History
Soapydoggo created this project
soap copied this project