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Home Mechanical Engineering IC Engines and Nuclear Power Plants Comments

  • Question
  • The thermal efficiency of diesel engines on weak mixtures is


  • Options
  • A. unaffected
  • B. lower
  • C. higher
  • D. dependent on other factors

  • Correct Answer
  • higher 


  • IC Engines and Nuclear Power Plants problems


    Search Results


    • 1. Reactors for propulsion applications are designed for

    • Options
    • A. any form of uranium
    • B. natura uranium
    • C. enriched uranium
    • D. plutonium
    • Discuss
    • 2. The detonating tendency in petrol engines increases with increase of compression ratio.

    • Options
    • A. True
    • B. False
    • Discuss
    • 3. The secondary fuel used in nuclear power plants is

    • Options
    • A. U233 and Pu239
    • B. U235 and Th232
    • C. U235 and Pu238
    • D. U233 and Pu238
    • Discuss
    • 4. The injection pressure in a diesel engine is about

    • Options
    • A. 10 bar
    • B. 100 bar
    • C. 150 bar
    • D. 500 bar
    • Discuss
    • 5. In a diesel engine, the duration between the time of injection and ignition, is known as

    • Options
    • A. pre-ignition period
    • B. delay period
    • C. period of ignition
    • D. burning period
    • Discuss
    • 6. 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
    • 7. 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
    • 8. The increase in pressure in a roots blower is entirely due to back flow of air.

    • Options
    • A. Agree
    • B. Disagree
    • Discuss
    • 9. 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
    • 10. 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


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