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Compressors, Gas Turbines and Jet Engines

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

Brayton or Atkinson cycle
Ericsson cycle
Rankine cycle
Carnot 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
p₂/p₁ = p₃/p₂ = p₄/p₃
p₃/p₁ = p₄/p₂

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Compressors, Gas Turbines and Jet Engines
The pressure and temperature conditions of air at the suction of compressor are

Slightly more than atmospheric
Slightly less than atmospheric
Atmospheric
Pressure slightly less than atmospheric and temperature slightly more than atmospheric

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Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

50: 1.
15: 1
30: 1
7: 1

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In a single phase
In three phases
In two phases
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered in a medium capacity air compressor per unit time is

0.1 to 1.2 m³/s
Above 5 m³/s
None of these
0.15 to 5 m³/s

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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