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Compressors, Gas Turbines and Jet Engines

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

Equal to
None of these
More than
Less than

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Compressors, Gas Turbines and Jet Engines
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

(v₁ - v₂)²/g
(v₁² -v₂²)/g
(v₁² -v₂²)/2g
(v₁ - v₂)²/2g

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are used for delivering

Small quantities of air at low pressures
Large quantities of air at high pressures
Small quantities of air at high pressures
Large quantities of air at low pressures

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At very high speed
At average speed
At zero speed
At very slow speed

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To cool the air during compression
To cool the air at delivery
To minimize the work of compression
To enable compression in two stages

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Compressors, Gas Turbines and Jet Engines
For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

Maximum cycle temperature alone
Both pressure ratio and maximum cycle temperature
Minimum cycle temperature alone
Pressure ratio alone

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