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Compressors, Gas Turbines and Jet Engines

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

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Compressors, Gas Turbines and Jet Engines
The clearance volume of the air compressor is kept minimum because

It greatly affects volumetric efficiency
It permits isothermal compression
It allows maximum compression to be achieved
It results in minimum work

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Compressors, Gas Turbines and Jet Engines
A centrifugal compressor works on the principle of

Conversion of kinetic energy into pressure energy
Centripetal action
Conversion of pressure energy into kinetic energy
Generating pressure directly

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Vacuum
Back to the compressor
Discharge nozzle
Atmosphere

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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
The ratio of the air actually delivered to the amount of piston displacement
Reciprocal of compression ratio

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

in the center
between ~ to i of the blade height
at the tip
at the base

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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