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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Atmospheric
Lowest
Anything
Highest

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Directly proportional to clearance volume
Inversely proportional to clearance volume
Not affected by clearance volume
Greatly affected by clearance volume

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More power
More/less power depending on other factors
Same power
Less power

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Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

0.53 kg/cm²
1.03 kg/cm²
1.00 kg/cm²
1.06 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

between ~ to i of the blade height
at the tip
at the base
in the center

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

Carnot cycle
Rankine cycle
Joule cycle
Ericsson cycle

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