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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

0.53 kg/cm²
1.06 kg/cm²
1.00 kg/cm²
1.03 kg/cm²

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

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

Same
More
None of the listed here
Less

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

All of these
Higher volumetric efficiency
Decreased discharge temperature
Lower power consumption per unit of air delivered

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Compressors, Gas Turbines and Jet Engines
In the aircraft propellers

Its functioning does not depend on presence of air
Propulsive matter is ejected from within the propelled body
All of these
The propulsive matter is caused to flow around the propelled body

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

Stainless steel
Carbon steel
High nickel alloy
High alloy steel

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