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
Posted: Wed May 18, 2022 4:47 pm
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.