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lidiya [134]
3 years ago
7

A turbine produces shaft power from a gas that enters the turbine with a (static) temperature of 628 K, a velocity of 143 m/s an

d a stagnation pressure of 14 atm. The gas exits the turbine with a stagnation temperature of 275 K and a stagnation pressure of 0.95 atm. The gas passing through the turbine has a molecular weight of 16 and a specific heat ratio of 1.45. What is the stagnation temperature of the gas entering the turbine? Assuming the turbine is adiabatic, is it also reversible?

Engineering
1 answer:
drek231 [11]3 years ago
7 0

Answer:

Explanation:

The detailed step by step calculation and appropriate formula is as shown in the attached file.

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