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  • Question
  • If V1 is the jet velocity and V0 is the vehicle velocity, then the propulsive efficiency of a rocket is given by


  • Options
  • A. If V1 is the jet velocity and V0 is the vehicle velocity, then the propulsive efficiency of a rocket
  • B. If V1 is the jet velocity and V0 is the vehicle velocity, then the propulsive efficiency of a rocket
  • C. If V1 is the jet velocity and V0 is the vehicle velocity, then the propulsive efficiency of a rocket
  • D. If V1 is the jet velocity and V0 is the vehicle velocity, then the propulsive efficiency of a rocket

  • Correct Answer
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  • IC Engines and Nuclear Power Plants problems


    Search Results


    • 1. The frictional power (F.P.) is given by

    • Options
    • A. F.P. = B.P. - I.P.
    • B. F.P. = I.P. - B.P.
    • C. F.P. = B.P./I.P.
    • D. F.P. = I.P./B.P.
    • Discuss
    • 2. The ratio of the brake power to the indicated power is called

    • Options
    • A. mechanical efficiency
    • B. overall efficiency
    • C. indicated thermal efficiency
    • D. volumetric efficiency
    • Discuss
    • 3. A supercharged engine as compared to an ordinary engine

    • Options
    • A. requires smaller foundation
    • B. is lighter
    • C. consumes less lubricating oil
    • D. all of these
    • Discuss
    • 4. For the same maximum pressure and heat input, the exhaust temperature of petrol engine is __________ than that of diesel engine.

    • Options
    • A. less
    • B. more
    • Discuss
    • 5. A turbo-jet does not require a turbine to drive the compressor.

    • Options
    • A. True
    • B. False
    • Discuss
    • 6. The theoretically correct mixture of air and petrol is

    • Options
    • A. 10:1
    • B. 15:1
    • C. 20:1
    • D. 25:1
    • Discuss
    • 7. The colour of exhaust from diesel engine is generally

    • Options
    • A. white
    • B. bluish
    • C. black
    • D. violent
    • Discuss
    • 8. The advancing of spark timing in spark ignition engines will __________ knocking tendency.

    • Options
    • A. increase
    • B. reduce
    • C. not effect
    • Discuss
    • 9. Uranium has isotopes

    • Options
    • A. U234
    • B. U235
    • C. U238
    • D. all of these
    • Discuss
    • 10. The maximum propulsive efficiency of a turbo-jet engine is at a speed of

    • Options
    • A. 1000 km/h
    • B. 2000 km/h
    • C. 2400 km/h
    • D. 3000 km/h
    • Discuss


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