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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Euler
Compressor efficiency
Pressure coefficient
Isentropic efficiency

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

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

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Radial flow compressors
All of these
Axial flow compressors
Pumps

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor

Increases with decrease in compression ratio
Decreases with increase in compression ratio
Decreases with decrease in compression ratio
Increases with increase in compression ratio

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Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

None of the listed here
Radial
Forward curved
Backward curved

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

After receiver
After inter-cooler
Between after-cooler and air receiver
Before inter-cooler

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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