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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

(W₁ + W₂)/W₁
(W₁ + W₂)/W₂
W₂/(W₁ + W₂)
W₁/(W₁ + W₂)

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Compressors, Gas Turbines and Jet Engines
In a reciprocating air compressor, the compression work per kg of air

Increases as clearance volume decreases
Decreases as clearance volume increases
Is independent of clearance volume
Increases as clearance volume increases

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Higher volumetric efficiency
Lower power consumption per unit of air delivered
All of these
Decreased discharge temperature

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Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isothermal compression
None of the listed here
Polytropic compression
Isentropic compression

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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

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

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Compressors, Gas Turbines and Jet Engines
The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

0.042361111111111
0.045833333333333
0.084027777777778
0.16736111111111

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