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Fluid flow analysis around an airfoil at low speed of 30m/s at 5 degree angle of attack(AOA). Previous tests on airfoil with 300 m/s at 0 degree AOA gave lift and drag coeefficients that are off-could be because of the incompressuble flow analysis. - Copy
by simscalesimscale
Nidish createdthis project
about 1 month ago
AroundEarth copied this project
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