Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Compressor pressure ratio
Inlet pressure to exhaust pressure
Pressures across the turbine
Highest pressure to exhaust pressure

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Compressors, Gas Turbines and Jet Engines
For a two stage reciprocating compressor, compression from p₁ to p₃ is with perfect intercooling and no pressure losses. If compression in both the cylinders follows the same polytropic process and the atmospheric pressure is pa, then the intermediate pressure p₂ is given by

p₂ = p₁. p₃
p₂ = Pa p₃/p₁
P₂ = Pa × p₃/p₁
p₂ = (p₁ + p₃)/2

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