Problem 6 10 points Bonus Air flows adiabatically through a frictional variable area duct divergent...
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Problem 6 10 points Bonus Air flows adiabatically through a frictional variable area duct divergent nozzle The conditions at the inlet are M 0 2 Tt1 460K and Pt 600kPa If the ratio of the exit section to the inlet area is A A 1 4 and Pt2 333 3kPa determine the exit Mach number temperature and pressure
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