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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Increases
First increases and then decreases
Decreases
Remain same

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Reciprocating pump
Centrifugal pump
Sliding vane compressor
Turbine

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler work is known as

Work coefficient
Slip factor
Pressure coefficient
Polytropic reaction

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Compressors, Gas Turbines and Jet Engines
The process, which causes the air to enter the impeller blades of a centrifugal compressor at ________ velocity (without effecting the mass of air to flow and velocity of flow) is known as prewhirl.

Reduced
None of these
Zero
Increased

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Inlet pressure to exhaust pressure
Pressures across the turbine
Compressor pressure ratio
Highest pressure to exhaust pressure

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between
Mechanical balance is better
Better lubrication is possible advantages of multistage

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