A test model is placed in the test section of a subsonic wind tunnel with a test-section to inlet nozzle area ratio of 0
Posted: Sun May 15, 2022 11:37 pm
A test model is placed in the test section of a subsonic wind tunnel with a test-section to inlet nozzle area ratio of 0.145. If the free-stream velocity inside the test section is 95 m/s calculate the pressure difference (in N/m/2) between the nozzle and test-section. Assume standard sea level conditions and select the closest answer 158 58 29 129 87