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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Increase of work ratio
Both (A) and (B) above
Decrease of thermal efficiency
Decrease of work ratio

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Compressors, Gas Turbines and Jet Engines
Open cycle gas turbine works on

Ericsson cycle
Brayton or Atkinson cycle
Carnot cycle
Rankine cycle

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

p₁ p₂ = p₃ p₄
p₁ p₃ = p₂ p₄
p₃/p₁ = p₄/p₂
p₂/p₁ = p₃/p₂ = p₄/p₃

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

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

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

They can generate very high thrust
They are not air breathing engines
These engines can work on several fuels
They have high propulsion efficiency

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

None of the listed here
Radial flow type
Centrifugal type
Axial flow type

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