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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is perpendicular to its axis, then it is a

Reciprocating compressor
Axial flow compressor
Turbo compressor
Centrifugal compressor

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Compressors, Gas Turbines and Jet Engines
If V, U and Vr represent the absolute velocity of fluid, velocity of blade, and relative velocity of fluid, and suffix ‘I’ and ‘o’ stand for entry and exit conditions, then in a rotary machine whose degree of reaction is unity

U < Vo
V = Uo
Vi = Vo
Vt > Vo

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In two phases
In the form of air and water mixture
In three phases
In a single phase

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Compressors, Gas Turbines and Jet Engines
For maximum work, the reheating should be done to an intermediate pressure of (Where p₁ = Maximum pressure, and p₂ = Minimum pressure)

(p₁ + p₂)/2
(p₁ - p₂)/2
p₁/p₂
p₁ p₂

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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
Gas turbine blades are given a rake

Depending on the velocity
In the direction of motion of blades
Equal to zero
Opposite to the direction of motion of blades

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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