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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Plasma
Liquid
Solids
Highly heated atmospheric air

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isothermally
Adiabatically
Isentropically
Isochronically

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

Liquid hydrogen
Kerosene
High speed diesel oil
Methyl alcohol

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Compressors, Gas Turbines and Jet Engines
If the clearance ratio for a reciprocating air compressor is 'K', then its volumetric efficiency is given by

1 - k + k (p₁/p₂)1/n
1 + k - k (p₂/p₁) n-1/n
1 - k + k (p₁/p₂) n- 1/n
1 + k - k (p₂/p₁)1/n

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Increases thermal efficiency
Allows operation at very high altitudes
Decreases heat loss is exhaust
Allows high compression ratio

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and net work output
Work done by turbine and heat supplied
Net work output and heat supplied
Net work output and work done by turbine

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