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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

Same
More
Less
More/less depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isochronically
Isothermally
Isentropically
Adiabatically

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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)

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

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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
Work factor
Pressure coefficient
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

Index of compressor performance
The ratio of stroke volume to clearance volume
Reciprocal of compression ratio
The ratio of the air actually delivered to the amount of piston displacement

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

High nickel alloy
High alloy steel
Stainless steel
Carbon steel

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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