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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Isothermal H.P/indicated H.R
Total output/air input
Isothermal H.P./shaft H.R
Compression work/motor input

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Cause moisture and oil vapour to drop out
Decrease the delivery temperature for ease in handling
Reduce volume
Cool the air

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

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

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Same
Zero
Less
More

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Compressors, Gas Turbines and Jet Engines
The material commonly used for air craft gas turbine is

Timken, Haste alloys
Duralumin
Stainless steel
High alloy steel

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Compressors, Gas Turbines and Jet Engines
Ramjet engine

Requires no air for its operation
Is not self operating at zero flight speed
Produces a jet consisting of plasma
Is self operating at zero flight speed

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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