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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
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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University Physics with Modern Physics
Authors: Hugh D. Young, Roger A. Freedman, Lewis Ford
12th Edition
ISBN: 978-0321501479, 9780805321876, 321501470, 978-0321501219
