9. An aircraft cruises at 270 m/s at 10,000 m where atmospheric pressure is 26430 Pa, p=0.4 kg/mº and y = 1.4. Calculate
Posted: Sun May 15, 2022 9:12 pm
9. An aircraft cruises at 270 m/s at 10,000 m where atmospheric pressure is 26430 Pa, p=0.4 kg/mº and y = 1.4. Calculate the Mach number the aircraft is cruising at and specify whether it is (5 marks) in a subsonic, transonic, or supersonic regime.