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Aerodynamic Study of Model Plane

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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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Project History

  • drodriguez32

    drodriguez32 created this project

  • adityask44

    adityask44 copied this project