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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

Small frontal area and high h.p.
High speed and high h.p.
Low weight and small frontal area
High h.p. and low weight

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

Pressure coefficient
Compressor efficiency
Isentropic efficiency
Euler

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

Reduce volume of air
Cool the air
Remove impurities from air
Cause moisture and oil vapour to drop out

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Greatly affected by clearance volume
Inversely proportional to clearance volume
Not affected by clearance volume
Directly proportional to clearance volume

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

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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