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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Remain same
Decrease
Does not change
Increase

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

200°C
500°C
700°C
1000°C

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

None of the listed here
Back pressure
Critical pressure
Discharge pressure

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the branch connections from compressed air lines should be taken from

Left side of main
Top side of main
Bottom side of main
Right side of main

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Carries its own oxygen
Uses compressed atmospheric air
Does not require oxygen
Uses surrounding air

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

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

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