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Compressors, Gas Turbines and Jet Engines

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

High nickel alloy
Stainless steel
Carbon steel
High alloy steel

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Highest pressure to exhaust pressure
Compressor pressure ratio
Pressures across the turbine
Inlet pressure to exhaust pressure

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

Same
Less
More
May be less or more depending on ambient conditions

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Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Open cycle
Closed cycle & Open cycle
Closed/open depending on other considerations
Closed cycle

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

60 to 70%
40 to 60%
10 to 40%
70 to 90%

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

Pressure coefficient
Euler
Isentropic efficiency
Compressor efficiency

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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