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Home Mechanical Engineering Compressors, Gas Dynamics and Gas Turbines Comments

  • Question
  • The maximum combustion pressure in gas turbine is __________ as compared to I.C. engine.


  • Options
  • A. more
  • B. less

  • Correct Answer
  • less 


  • Compressors, Gas Dynamics and Gas Turbines problems


    Search Results


    • 1. A rotary compressor is driven by an

    • Options
    • A. electric motor
    • B. engine
    • C. either (a) or (b)
    • D. none of these
    • Discuss
    • 2. In the aircraft propellers

    • Options
    • A. the propulsive matter is ejected from within the propelled body
    • B. the propulsive matter is caused to flow around the propelled body
    • C. its functioning does not depend upon the presence of air
    • D. none of the above
    • Discuss
    • 3. Which of the following statement is wrong?

    • Options
    • A. In a two stage reciprocating air compressor with complete intercooling, maximum work is saved.
    • B. The minimum work required for a two stage reciprocating air compressor is double the work required for each stage.
    • C. The ratio of the volume of free air delivery per stroke to the swept volume of the piston is called volumetric efficiency.
    • D. none of the above
    • Discuss
    • 4. Gas turbine as compared to steam turbine

    • Options
    • A. requires less space for installation
    • B. has compressor and combustion chamber
    • C. has less efficiency
    • D. all of these
    • Discuss
    • 5. The maximum delivery pressure in a rotary air compressor is

    • Options
    • A. 10 bar
    • B. 20 bar
    • C. 30 bar
    • D. 50 bar
    • Discuss
    • 6. The efficiency of a jet engine is higher at

    • Options
    • A. low speeds
    • B. high speeds
    • C. low altitudes
    • D. high altitudes
    • Discuss
    • 7. An open cycle gas turbine works on the same cycle as that of a closed cycle gas turbine.

    • Options
    • A. Yes
    • B. No
    • Discuss
    • 8. The maximum temperature in a gas turbine is

    • Options
    • A. 200°C
    • B. 500°C
    • C. 700°C
    • D. 1000°C
    • Discuss
    • 9. In a jet propulsion

    • Options
    • A. the propulsive matter is ejected from within the propelled body
    • B. the propulsive matter is caused to flow around the propelled body
    • C. its functioning does not depend upon presence of air
    • D. none of the above
    • Discuss
    • 10. An aftercooler is used to

    • Options
    • A. remove impurities from air
    • B. reduce volume of air
    • C. cause moisture and oil vapour to drop out
    • D. cool the air
    • Discuss


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