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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Pick up wrong statement. Surging phenomenon in centrifugal compressor depends on

Pressure ratio
Change in load
Mass flow rate
Stagnation pressure at the outlet

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.

Outlet whirl velocity
Inlet whirl velocity
Outlet velocity of flow
Inlet velocity of flow

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Carnot cycle
Brayton or Atkinson cycle
Rankine cycle
Ericsson cycle

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Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Slip factor
Pressure coefficient
Degree of reaction
Work factor

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

All of the listed here
Produces uniform torque
Can be driven at a very high speed
Has more efficiency

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

Same
May be less or more depending on ambient conditions
More
Less

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