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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

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

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Depends on other factors
More
Same
Less

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

700°C
1000°C
200°C
500°C

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

Carbon steel
High alloy steel
Stainless steel
High nickel alloy

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Decreases the thermal efficiency
Increases the thermal efficiency
Increases the turbine work
Increases the compressor work

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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