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300 Important Compressors, Gas Turbines And Jet Engines MCQ Question and Answer | PDF Free Download

Compressors, Gas Turbines And Jet Engines MCQ Question and Answer PDF Free Download

1.Actual compression curve is

  • ASame as isothermal
  • BSame as adiabatic
  • CBetter than isothermal and adiabatic
  • DIn between isothermal and adiabatic
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Correct Answer : (D)

In between isothermal and adiabatic

Explanation:

2.Work ratio of a gas turbine plant is ratio of

  • ANet work output and work done by turbine
  • BNet work output and heat supplied
  • CWork done by turbine and heat supplied
  • DWork done by turbine and net work output
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Correct Answer : (A)

Net work output and work done by turbine

Explanation:

3.In a reciprocating air compressor, the compression work per kg of air

  • AIncreases as clearance volume increases
  • BDecreases as clearance volume increases
  • CIs independent of clearance volume
  • DIncreases as clearance volume decreases
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Correct Answer : (C)

Is independent of clearance volume

Explanation:

4.The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called

  • ACompressor efficiency
  • BVolumetric efficiency
  • CIsothermal efficiency
  • DMechanical efficiency
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Correct Answer : (D)

Mechanical efficiency

Explanation:

5.A large clearance volume in a reciprocating compressor results in

  • AReduced volume flow rate
  • BIncreased volume flow rate
  • CLower suction pressure
  • DLower delivery pressure
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Correct Answer : (A)

Reduced volume flow rate

Explanation:

6.Diffuser in a compressor is used to

  • AIncrease velocity
  • BMake the flow streamline
  • CConvert pressure energy into kinetic energy
  • DConvert kinetic energy into pressure energy
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Correct Answer : (D)

Convert kinetic energy into pressure energy

Explanation:

7.Pick up wrong statement. Surging phenomenon in centrifugal compressor depends on

  • AMass flow rate
  • BPressure ratio
  • CChange in load
  • DStagnation pressure at the outlet
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Correct Answer : (D)

Stagnation pressure at the outlet

Explanation:

8.Losses in a centrifugal compressor are due to

  • AInlet losses
  • BImpeller channel losses
  • CDiffuser losses
  • DAll of the above
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Correct Answer : (D)

All of the above

Explanation:

9.The volumetric efficiency for reciprocating air compressors is about

  • A10 to 40%
  • B40 to 60%
  • C60 to 70%
  • D70 to 90%
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Correct Answer : (D)

70 to 90%

Explanation:

10.Cylinder clearance in a compressor should be

  • AAs large as possible
  • BAs small as possible
  • CAbout 50% of swept volume
  • DAbout 100% of swept volume
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Correct Answer : (B)

As small as possible

Explanation:

11.Axial flow compressor resembles

  • ACentrifugal pump
  • BReciprocating pump
  • CTurbine
  • DSliding vane compressor
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Correct Answer : (C)

Turbine

Explanation:

12.The ratio of work done per cycle to the swept volume in case of compressor is called

  • ACompression index
  • BCompression ratio
  • CCompressor efficiency
  • DMean effective pressure
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Correct Answer : (D)

Mean effective pressure

Explanation:

13.The absolute pressure of air at the outlet of a compressor is called

  • ABack pressure
  • BCritical pressure
  • CDischarge pressure
  • DNone of these
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Correct Answer : (C)

Discharge pressure

Explanation:

14.Rotary compressor is best suited for

  • ALarge quantity of air at high pressure
  • BSmall quantity of air at high pressure
  • CSmall quantity of air at low pressure
  • DLarge quantity of air at low pressure
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Correct Answer : (B)

Small quantity of air at high pressure

Explanation:

15.Reciprocating air compressor is best suited for

  • ALarge quantity of air at high pressure
  • BSmall quantity of air at high pressure
  • CSmall quantity of air at low pressure
  • DLarge quantity of air at low pressure
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Correct Answer : (B)

Small quantity of air at high pressure

Explanation:

16.In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

  • A1 bar
  • B16 bar
  • C64 bar
  • D256 bar
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Correct Answer : (C)

64 bar

Explanation:

17.In air breathing jet engine, the jet is formed by expanding

  • AHighly heated atmospheric air
  • BSolids
  • CLiquid
  • DPlasma
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Correct Answer : (A)

Highly heated atmospheric air

Explanation:

18.Volumetric efficiency is

  • AThe ratio of stroke volume to clearance volume
  • BThe ratio of the air actually delivered to the amount of piston displacement
  • CReciprocal of compression ratio
  • DIndex of compressor performance
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Correct Answer : (B)

The ratio of the air actually delivered to the amount of piston displacement

Explanation:

19.The blades of gas turbine are made of

  • AHigh nickel alloy
  • BStainless steel
  • CCarbon steel
  • DHigh alloy steel
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Correct Answer : (A)

High nickel alloy

Explanation:

20.Ramjet engine

  • AIs self operating at zero flight speed
  • BIs not self operating at zero flight speed
  • CRequires no air for its operation
  • DProduces a jet consisting of plasma
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Correct Answer : (B)

Is not self operating at zero flight speed

Explanation: