What is the typical compression ratio found in a gas turbine?

Compressors, Gas Turbines and Jet Engines MCQs for PPSC, FPSC, NTS, and Pakistan government job tests. Select an option below, then read the explanation.

Compressors, Gas Turbines and Jet Engines

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Subject
Compressors, Gas Turbines and Jet Enginesmechanical-engineering-mcqs › compressors-gas-turbines-and-jet-engines
Published
23 Jan 2019
Last updated
28 May 2026

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Explanation

The compression ratio in gas turbines generally falls around 8:1, meaning the air is compressed to eight times its original pressure before combustion.

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