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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isothermal compression
None of the listed here
Isentropic compression
Polytropic compression

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Compressors, Gas Turbines and Jet Engines
Isothermal compression though most efficient, but is not practicable because

Compressor has to run at very slow speed to achieve it
It is impossible in practice
It requires very big cylinder
It does not increase pressure much

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

Minimum cycle temperature
Pressure ratio
All of these
Maximum cycle temperature

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

Pressure coefficient
Polytropic reaction
Slip factor
Work coefficient

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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
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

0.5%
0.1%
1.0%
5%

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