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Compressors, Gas Turbines and Jet Engines

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

More
Zero
Same
Less

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Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

Less
Zero
More
Same

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio in gas turbines

Do not damage turbine blades
Reduces exhaust temperature
Improves thermal efficiency
Increases power output

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Increased inclination of chord with air steam
Reducing mass flow rate with increase in pressure ratio
Fixed mass flow rate regardless of pressure ratio
No flow of air

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Compressors, Gas Turbines and Jet Engines
The efficiency of roots blower ________ with the increase in pressure ratio.

Decreases
Does not change
None of these
Increases

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Compressors, Gas Turbines and Jet Engines
The pressure ratio in gas turbines is of the order of

0.37569444444444
2.5423611111111
0.084027777777778
0.16736111111111

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