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Physics, 04.11.2021 19:30 hfleysher

Consider a wing mounted in the test section of a subsonic wind tunnel. The velocity of the airflow is 160 ft/s. If the velocity at a point on the wing is 195 ft/s, what is the pressure coefficient at this point

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