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Compressors, Gas Turbines and Jet Engines

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

None of these
Same
Lower
Higher

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

Carnot cycle
Rankine cycle
Ericsson cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber and incidence angle
Space-chord ratio
Blade camber
Blade camber and space-chord ratio

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High speed and high h.p.
Small frontal area and high h.p.
Low weight and small frontal area
High h.p. and low weight

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

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

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

No air stream
One air stream
Solid fuel firing
Two or more air streams

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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