Engineering, 12.03.2020 03:33 robertsabbiegale

Consider a wing mounted in the test-section of a subsonic wind tunnel. The velocity of the airflow is 160 ft/s, and the velocity at a point on the wing is 293 ft/s.

If the test-section air temperature is 510°R and the flow velocity is increased to 450 ft/s, what is the pressure coefficient at the same point?

(Round the final answer to three decimal places.)

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Consider a wing mounted in the test-section of a subsonic wind tunnel. The velocity of the airflow i...