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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Increases
Decreases
Remain constant
First decreases and then increases

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

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

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

More
Same
More/less depending on compressor capacity
Less

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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)/2
p₁ p₂
(p₁ - p₂)/2
p₁/p₂

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Before the inter-cooler
Before first stage suction
After the inter-cooler
Between the after-cooler and receiver

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Minimum cycle temperature
All of these
Maximum cycle temperature
Pressure ratio

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