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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Diffuser inlet radius
Impeller outlet radius
Diffuser outlet radius
Impeller inlet radius

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered in a medium capacity air compressor per unit time is

0.15 to 5 m³/s
0.1 to 1.2 m³/s
Above 5 m³/s
None of these

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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)/2
(p₁ - p₂)/2
p₁ p₂

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Compressors, Gas Turbines and Jet Engines
A jet engine has

No propeller
Propeller on the top
Propeller in front
Propeller at back

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Compressors, Gas Turbines and Jet Engines
The clearance volume of the air compressor is kept minimum because

It permits isothermal compression
It greatly affects volumetric efficiency
It allows maximum compression to be achieved
It results in minimum work

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

None of these
Decrease
Increase
Remain same

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