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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

Multi cylinder engine
4-stroke petrol engine
4-stroke diesel engine
Gas turbine

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

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

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Compressors, Gas Turbines and Jet Engines
For maximum work, the reheating should be done to an intermediate pressure of (Where p₁ = Maximum pressure, and p₂ = Minimum pressure)

p₁/p₂
p₁ p₂
(p₁ - p₂)/2
(p₁ + p₂)/2

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Lower
Can't be compared
Higher
Equal

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

Stainless steel
High nickel alloy
Carbon steel
High alloy steel

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Reducing mass flow rate with increase in pressure ratio
Increased inclination of chord with air steam
No flow of air
Fixed mass flow rate regardless of pressure ratio

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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