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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isothermally
Adiabatically
Isentropically
Isochronically

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Compressors, Gas Turbines and Jet Engines
The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)

(v₁ - v₂)²/2g
(v₁² -v₂²)/g
(v₁ - v₂)²/g
(v₁² -v₂²)/2g

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Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

As small as possible
About 100% of swept volume
As large as possible
About 50% of swept volume

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance, the work-done on the air during isentropic compression is ________ the heat required to raise the temperature of air from T₁ to T₂ at a constant pressure.

Greater than
Equal to
Less than
None of these

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Compressors, Gas Turbines and Jet Engines
During peak load periods, the best method of controlling compressors is

Constant speed unloader
Start-stop motor
Variable speed
Relief valve

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as isothermal
Better than isothermal and adiabatic
Same as adiabatic
In between isothermal and adiabatic

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