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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)

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

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during

Polytropic compression
None of these
Isentropic compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Chemical rocket engine
A propeller system
Gas turbine engine equipped with a propulsive nozzle and diffuse
Ramjet engine

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Multistage compression with intercooling
Multistage compression without intercooling
None of these
Single stage compression

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Uses compressed atmospheric air
Uses surrounding air
Carries its own oxygen
Does not require oxygen

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Results in saving of power in compressing a given volume to given pressure
Enables compression in two stages
Is the standard practice for big compressors
Cools the delivered air

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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