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Engineering, 02.03.2020 18:49 Britny2386

You are working as a flight-test engineer and during the low-speed phase of the test program for the X-37, you know that the plane is flying at an altitude of 8 km. The pressure at gage 1 is 1550 N/m2 , gage; the pressure at gage 2 is -3875 N/m2 , gage. a. If gage 1 is known to be at the stagnation point, what is the velocity of the airplane

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