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Compressors, Gas Turbines and Jet Engines

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

Work coefficient
Slip factor
Pressure coefficient
Polytropic reaction

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

Pressure ratio
Minimum cycle temperature
Maximum cycle temperature
All of these

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

Compressor efficiency
Pressure coefficient
Euler
Isentropic efficiency

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

700°C
200°C
500°C
1000°C

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Compressors, Gas Turbines and Jet Engines
The inter-cooler pressure, for minimum work required, for a two stage reciprocating air compressor, is given by (where p₁ = Intake pressure of air, p₂ = Inter-cooler pressure, and p₃ = Delivery pressure of air)

p₂ = p₁ × p₂
p₂ = p₁ × p₃
p₂ = p₃/p₁
p₂ = p₁/p₃

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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

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

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