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SOLVED: Air enters a constant-area duct at Mach 3 and stagnation conditions 750 K and 1.3 MPa. In the duct, it undergoes a frictionless energy-transfer process such that the exit Mach number is unity. Consider two cases: a normal shock at the inlet to the duct and (b) shock-free supersonic heating. Determine the stagnation temperature and pressure at the exit in each case. Is there two cases?M = 1M1 = 3To1 = 750 KPo1 = 1.3 MPah1 =
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