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  • Question

  • The efficiency of a gas turbine is given by


  • Options
  • A. The efficiency of a gas turbine is given by
  • B. The efficiency of a gas turbine is given by
  • C. The efficiency of a gas turbine is given by
  • D. The efficiency of a gas turbine is given by

  • Correct Answer
  •  

    • Thermodynamics problems

    Search Results

    • 1. In closed cycle gas turbine, the air is compressed

    • Options
    • A. isothermally
    • B. isentropically
    • C. polytropically
    • D. none of these
      • Discuss
    • 2. In a free expansion process,

    • Options
    • A. W1 - 2 = 0
    • B. Q1 - 2 = 0
    • C. dU = 0
    • D. all of these
      • Discuss
    • 3. By decreasing the highest temperature in the Carnot cycle, its efficiency is increased.

    • Options
    • A. True
    • B. False
      • Discuss
    • 4. One kg of carbon requires 8/3 kg of oxygen for its complete combustion and produces 11/3 kg of carbon dioxide gas.

    • Options
    • A. Agree
    • B. Disagree
      • Discuss
    • 5. The increase in entropy of a system represents

    • Options
    • A. increase in availability of energy
    • B. increase in temperature
    • C. decrease in pressure
    • D. degradation of energy
      • Discuss
    • 6. Boyle's law states that change of internal energy of a perfect gas is directly proportional to the change of temperature.

    • Options
    • A. Agree
    • B. Disagree
      • Discuss
    • 7. A process, in which the gas is heated or expanded in such a way that product of its pressure and volume remains constant, is called isothermal process.

    • Options
    • A. Yes
    • B. No
      • Discuss
    • 8. The temperature at which the volume of a gas becomes zero is called

    • Options
    • A. absolute scale of temperature
    • B. absolute zero temperature
    • C. absolute temperature
    • D. none of these
      • Discuss
    • 9. One reversible heat engine operates between 1600 K and T2 K and another reversible heat engine operates between T2 K and 400 K. If both the engines have the same heat input and output, then temperature T2 is equal to

    • Options
    • A. 800K
    • B. 1000K
    • C. 1200K
    • D. 1400K
      • Discuss
    • 10. The work ratio of a gas turbine plant is given by

    • Options
    • A.
    • B.
    • C.
    • D.
      • Discuss

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