A wing is mounted in the test section of a subsonic wind tunnel. The velocity of the free-stream airflow is 180 ft/s. T

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answerhappygod
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A wing is mounted in the test section of a subsonic wind tunnel. The velocity of the free-stream airflow is 180 ft/s. T

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A wing is mounted in the test section of a subsonic wind tunnel. The velocity of the free-stream airflow is 180 ft/s. The pressure coefficient at a point on the airfoil is -0.234567. Determine the velocity of the flow at that point on the wing.
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