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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)

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

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Compressors, Gas Turbines and Jet Engines
In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to

Intake temperature and pressure conditions
20°C and 1 kg/cm²
0°C and 1 kg/cm²
N.T.P. conditions

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the compressed air main line should

Be laid exactly horizontally
Drop gradually towards the point of use
Be laid vertically
Rise gradually towards the point of use

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

2.2 kg
1.0 kg
1.3 kg
0.5 kg

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

Centrifugal type
None of these
Radial flow type
Axial flow type

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Impeller outlet radius
Diffuser outlet radius
Impeller inlet radius
Diffuser inlet radius

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