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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

16 kg/cm²
25 kg/cm²
10 kg/cm²
6 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Adiabatic compression is one in which

Temperature rise follows a linear relationship
Work done is maximum
Temperature during compression remains constant
No heat leaves or enters the compressor cylinder during compression

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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
Impeller inlet radius
Diffuser outlet radius

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Cooling chamber
All of these
Heating chamber
Compressor

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Electric motor
None of these
Engine
Either (A) or (B)

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

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