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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

0.045833333333333
0.042361111111111
0.16736111111111
0.084027777777778

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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 does not increase pressure much
It requires very big cylinder
It is impossible in practice

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase speed
Increase temperature
Increase power output
Reduce turbine size

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

Reheating
All of the listed here
Inter cooling
Adding a regenerator

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Inlet losses
Impeller channel losses
Diffuser losses
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

kg/m²
m³/min
kg/m³
m³/kg

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