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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

10 kg/cm²
14.7 kg/cm²
6 kg/cm²
2 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

1 - (1/r) ɣ-1/ɣ
1 - (1/r) ɣ/ɣ-1
r ɣ-1
1 - r ɣ-1

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

0.1 bar and 40°C
0.1 bar and 20°C
1 bar and 40°C
1 bar and 20°C

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

The ratio of the air actually delivered to the amount of piston displacement
The ratio of stroke volume to clearance volume
Index of compressor performance
Reciprocal of compression ratio

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

Increases
Decreases
Has no effect on
None of these

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

kg/m²
kg/m³
m³/kg
m³/min

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