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Home Mechanical Engineering Compressors, Gas Dynamics and Gas Turbines Comments

  • Question
  • The compression ratio in a gas turbine is


  • Options
  • A. 4
  • B. 1
  • C. 9
  • D. 12

  • Correct Answer



  • Compressors, Gas Dynamics and Gas Turbines problems


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    • 1. The degree of reaction in an axial flow compressor is defined as the ratio of static enthalpy rise in the

    • Options
    • A. rotor to static enthalpy rise in the stator
    • B. stator to static enthalpy rise in the rotor
    • C. rotor to static enthalpy rise in the stage
    • D. stator to static enthalpy rise in the stage
    • Discuss
    • 2. A rocket works with maximum overall efficiency when air-craft velocity is __________ the jet velocity.

    • Options
    • A. equal to
    • B. one-half
    • C. double
    • Discuss
    • 3. The increase in pressure in a roots blower is entirely due to back flow of air.

    • Options
    • A. Agree
    • B. Disagree
    • Discuss
    • 4. Only rocket engines can be propelled to space because

    • Options
    • A. they can generate very high thrust
    • B. they have high propulsion efficiency
    • C. these engines can work on several fuels
    • D. they are not air-breathing engines
    • Discuss
    • 5. In diesel engines, the fuel is injected in the form of very fine spray, into the engine cylinder, which gets ignited due to high temperature of the compressed air.

    • Options
    • A. Agree
    • B. Disagree
    • Discuss
    • 6. The volume of air delivered by the compressor is called

    • Options
    • A. free air delivery
    • B. compressor capacity
    • C. swept volume
    • D. none of these
    • Discuss
    • 7. The compressed air may be used

    • Options
    • A. in gas turbine plants
    • B. for operating pneumatic drills
    • C. in starting and supercharging of I.C. engines
    • D. all of the above
    • Discuss
    • 8. The ratio of workdone per cycle to the stroke volume of the compressor is known as

    • Options
    • A. compressor capacity
    • B. compression ratio
    • C. compressor efficiency
    • D. mean effective pressure
    • Discuss
    • 9. Which of the following statement is correct?

    • Options
    • A. The ratio of the discharge pressure to the inlet pressure of air is called compressor efficiency.
    • B. The compression ratio for the compressor is always greater than unity.
    • C. The compressor capacity is the ratio of workdone per cycle to the stroke volume.
    • D. During isothermal compression of air, the workdone in a compressor is maximum.
    • Discuss
    • 10. The clearance volume in the compressor is kept minimum because it effects on volumetric efficiency.

    • Options
    • A. Correct
    • B. Incorrect
    • Discuss


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