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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
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
Soapydoggo created this project
about 2 years ago
soap copied this project
about 2 years ago