1.

Determine the jet exhaust velocity, if the flow has an exit Mach number of 3 and temperature of 700 K. (Assume γ= 1.4 and Cp = 1005 J/kgK)

A. 1591 m/s
B. 2041 m/s
C. 991 m/s
D. 781 m/s
Answer» B. 2041 m/s


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