Compressors, Gas Turbines and Jet Engines
In n₁ and n₂ are the indices of compression for the first and second stage of compression, then the ratio of work-done on the first and second stages (W₁/W₂) with perfect intercooling is given by

W₁/W₂ = n₁(n₂ - 1)/n₂(n₁ - 1)
W₁/W₂ = n₂(n₁ - 1)/n₁(n₂ - 1)
W₁/W₂ = n₁/n₂
W₁/W₂ = n₂/n₁

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion

None of these
Its functioning does not depend upon presence of air
The propulsive matter is caused to flow around the propelled body
The propulsive matter is ejected from within the propelled body

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