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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Fighter bombers use following type of engine

Ramjet
Rocket
Turbojet
Turbo-propeller

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

1000°C
500°C
700°C
200°C

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Compressors, Gas Turbines and Jet Engines
For supplying intermittent small quantity of air at high pressure, following compressor is best suited

Screw
Reciprocating
Centrifugal
Axial

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

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

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Higher
Same
Lower
None of these

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Increasing speed of incoming air
Compression of inlet air
Reduction of speed of incoming air and conversion of part of it into pressure energy
Lost work

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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