Compressors, Gas Turbines and Jet Engines
Ramjet engine

Is not self operating at zero flight speed
Produces a jet consisting of plasma
Is self operating at zero flight speed
Requires no air for its operation

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in gas turbine results in

Increase in both thermal efficiency and net output
Decrease in both thermal efficiency and net output
Increase in thermal efficiency but decrease in net output
Increase in net output but decrease in thermal efficiency

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Compressors, Gas Turbines and Jet Engines
If p₁ is the pressure of air entering the L.P, cylinder and p₃ is the pressure of air leaving the H.P. cylinder, then the ratio of cylinder diameters for a single acting, two stage reciprocating compressor with complete intercooling is given by

D₁/D₂ = (p₁/p₃)1/4
D₁/D₂ = (p₁ p₃)1/2
D₁/D₂ = (p₁ p₃)1/4
D₁/D₂ = (p₃/p₁)1/4

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