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Aerodynamic Study of Model Plane
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1 Geometry 1 Mesh 2 Simulation setups 1 Result
About this project
To investigate the behaviour of drag and lift, and look at velocity and pressure distribution across the wing for different angles of attack with an angle of 3 degrees, and 20 degrees for a plane travelling at 20 m/s
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drodriguez32 created this project
adityask44 copied this project