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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Ideal compression
Isothermal compression
Adiabatic compression
Isentropic compression

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

0.1 bar and 20°C
1 bar and 20°C
1 bar and 40°C
0.1 bar and 40°C

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Same
Higher
None of these
Lower

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

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Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Six times
Four times
Two times
Three times

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Compressors, Gas Turbines and Jet Engines
The thrust of a jet propulsion power unit can be increased by

All of these
Injecting water into the compressor
Injecting ammonia into the combustion chamber
Burning fuel after gas turbine

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