Seumas2302 Seumas2302
  • 13-09-2022
  • Engineering
contestada

A supersonic transport is flying at a velocity of 1500 mph at a standard altitude of50, 000 f t. 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 whereis this point on the wing most likely located?

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