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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

Forward curved
Backward curved
None of the listed here
Radial

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

Employing inter-cooler
By running compressor at very slow speed
By insulating the cylinder
By constantly cooling the cylinder

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Compressors, Gas Turbines and Jet Engines
Which is false statement about air receivers?

These act as reservoir to take care of sudden demands
These increase compressor efficiency
These are used to dampen pulsations
These knock out some oil and moisture

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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
(p₁ + p₂)/2

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow and decrease in efficiency
Increase in efficiency
Decrease in flow
Increase in flow

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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

Can't be compared
Higher
Equal
Lower

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