Problem 13.39 - psia Equations and Computations: Using the...

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Problem 13.39 [Difficulty: 1] Given: Hydrogen flow through a converging-diverging nozzle Find: Nozzle exit Mach number Solution: The given or available data is: R = 766.5 ft-lbf/lbm-°R k = 1.41 p 0 = 100 psia T 0 = 540 °F T 0 = 1000 °R p e = 20
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Unformatted text preview: psia Equations and Computations: Using the stagnation to exit static pressure ratio, we can find the exit Mach number: (using built-in function Isenp ( M , k )) M e = 1.706...
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This note was uploaded on 01/20/2012 for the course EGN 3353C taught by Professor Lear during the Fall '07 term at University of Florida.

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