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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a two stage compressor

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

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

Less
More
May be less or more depending on ambient conditions
Same

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Decrease
Other factors control it
Increase
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
The pressure of air at the beginning of the compression stroke is ___ the atmospheric pressure.

None of the listed here
Equal to
More than
Less than

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Compressors, Gas Turbines and Jet Engines
For slow speed large capacity compressor, following type of valve will be best suited

Disc or feather type
Any of the above
Mechanical valve of the Corliss, sleeve, rotary or semi rotary type
Poppet valve

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

m³/min
m³/kg
kg/m²
kg/m³

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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