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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.001
0.05
0.01
0.005

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

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

Slip factor
Polytropic reaction
Work coefficient
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating air compressor, without clearance, the compression of air may be

Isothermal
Polytropic
Any one of these
Isentropic

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Isothermal compression
Adiabatic compression
Ideal compression
Isentropic compression

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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

Degree of reaction
Slip factor
Pressure coefficient
Work factor

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