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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work ratio of simple gas turbine cycle depends on

Pressure ratio
Minimum cycle temperature
Maximum cycle temperature
All of these

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
Ramjet engine

Produces a jet consisting of plasma
Requires no air for its operation
Is self operating at zero flight speed
Is not self operating at zero flight speed

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Dependent on other factors
Higher
Same
Lower

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

Equal to
More than
None of these
Less than

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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