A supersonic transport is flying at a velocity of 1500 mph at a standard altitude of 50,000 ft. The temperature at a point on the wing is 439 K. Calculate the flow velocity and pressure at that point assuming isentropic flow. Based on your results where is this point on the wing most likely located?

Answer rating: 100% (QA)

Velocity of supersonic 1500 mph Standard altitude ... View the full answer