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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

Small frontal area and high h.p.
High speed and high h.p.
High h.p. and low weight
Low weight and small frontal area

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Diffuser inlet radius
Diffuser outlet radius
Impeller outlet radius
Impeller inlet radius

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

Work coefficient
Polytropic reaction
Pressure coefficient
Slip factor

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

Reheating
Inter cooling
Adding a regenerator
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

None of these
Equal to
Less than
More than

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Minimum cycle temperature
Maximum cycle temperature
Pressure ratio
All of these

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