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Compressors, Gas Turbines and Jet Engines

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
Work factor
Degree of reaction
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isothermal
Isochoric
Adiabatic
Isentropic

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Before the inter-cooler
Before first stage suction
After the inter-cooler
Between the after-cooler and receiver

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Reciprocating type
Axial flow type
Centrifugal type
Lobe type

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

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

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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