Compressors, Gas Turbines and Jet Engines - Mechanical Engineering Questions and Answers

Home / Mechanical Engineering / Compressors, Gas Turbines and Jet Engines :: Discussion

Pressure ratio in gas turbines is the ratio of

Compressor pressure ratio

Highest pressure to exhaust pressure

Inlet pressure to exhaust pressure

Pressures across the turbine

Answer : Option B

Explanation :

Pressure ratio in gas turbines is the ratio of Highest pressure to exhaust pressure

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