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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

1000°C
500°C
200°C
700°C

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

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Less
Zero
More
Same

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Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Mass
Linear momentum
Energy
Flow

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Multistage compression without intercooling
None of these
Multistage compression with intercooling
Single stage compression

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Compression ratio
None of these
Pressure ratio
Work ratio

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