Maurice Tutor

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Category > Management Posted 13 Oct 2017 My Price 4.00

validity of aerodynamic assumptions

To test the validity of aerodynamic assumptions made in the design of the aircraft, its model is being tested in a wind tunnel. The support bracket is connected to a force and moment balance, which is zeroed when there is no airflow. Under test conditions, the lift L, drag D, and pitching moment MG act as shown. The force balance records the lift, drag, and a moment MP. Determine MG in terms of L, D, and MP.

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Maurice Tutor
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Status NEW Posted 13 Oct 2017 05:10 PM My Price 4.00

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