A Manometer Connected To A Pitot Tube On An Aeroplane Registers A Gauge Pressure Of 23 Kpa The Local Pressure And Tempe 1 (66.52 KiB) Viewed 41 times
A manometer connected to a pitot tube on an aeroplane registers a gauge pressure of 23 kPa. The local pressure and temperature at the altitude of the aeroplane are 61.66 kPa and 262.2 K respectively. What is is the speed of the plane assuming incompressible flow? Give your answer in m/s.
A manometer connected to a pitot tube on an aeroplane registers a gauge pressure of 23 kPa. The local pressure and temperature at the altitude of the aeroplane are 61.66 kPa and 262.2 K respectively. What is the speed of the plane assuming compressible flow? Give your answer in m/s.
Join a community of subject matter experts. Register for FREE to view solutions, replies, and use search function. Request answer by replying!