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Category > Applied Sciences Posted 21 May 2017 My Price 5.00

To test the validity of aerodynamic assumptions made in the design

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 MGact 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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Alpha Geek
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Status NEW Posted 21 May 2017 02:05 PM My Price 5.00

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