If at a point along the isentropic rocket nozzle, the temperature of t – McqOptions

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1.	If at a point along the isentropic rocket nozzle, the temperature of the gas is 718 K, and the flow velocity is 150 m/s, determine the nozzle exit velocity, given the exhaust gas temperature is 460 K (Assume Cp = 1005 J/kg K)
A.	840.25 m/s
B.	735.58 m/s
C.	913.07 m/s
D.	374.95 m/s
Answer» C. 913.07 m/s

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