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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Average of the jet velocity
Twice the jet velocity
Half the jet velocity
Jet velocity

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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
Lower
None of these

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

2000°C
1500°C
700°C
1000°C

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Higher
Can't be compared
Lower
Equal

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Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a two stage compressor

p₁ = p₂ p3
p₁/p₃ = p₂/p₁
p₁ = p3
p₂/p₁ = p₃/p₂

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

After inter-cooler
Between after-cooler and air receiver
After receiver
Before inter-cooler

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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