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Problem 2 (30 points): Air flows through a duct shown below. If the flow in section I has a Mach number, M-2, A-20 pts)
Problem 2 (30 points): Air flows through a duct shown below. If the flow in section I has a Mach number, M-2, A-20 pts) Calculate the Mach numbers in sections 2, 3 and 4. B-10 pts) If static pressure in section 1 is, P1-5 atm, calculate the pressure, PA, in section 4. Hint: The waves shown in the duct are expansion waves. There are no compression (shock) waves. M=2 1 3 8 2 4
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Engineering Mechanics Statics
Authors: R. C. Hibbeler
12th Edition
136077900, 978-0136077909
