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Home Mechanical Engineering Compressors, Gas Dynamics and Gas Turbines Comments

  • Question
  • The compressor capacity will be __________ if the temperature of intake air is lowest.


  • Options
  • A. lowest
  • B. highest

  • Correct Answer
  • highest 


  • Compressors, Gas Dynamics and Gas Turbines problems


    Search Results


    • 1. Reheating in a gas turbine

    • Options
    • A. increases the thermal efficiency
    • B. increases the compressor work
    • C. increases the turbine work
    • D. decreases the thermal efficiency
    • Discuss
    • 2. In a centrifugal compressor, the air enters the impeller axially and leaves the vane radially.

    • Options
    • A. Yes
    • B. No
    • Discuss
    • 3. The intercooler pressure, for minimum work required, for a two stage reciprocating air compressor, is given by (where p1 = Intake pressure of air, p2 = Intercooler pressure, and p3 = Delivery pressure of air)

    • Options
    • A. p2 = p1 x p3
    • B. p2 = p1/p3
    • C. p2 = p1 x p3
    • D. p2 = p3/p1
    • Discuss
    • 4. The performance of air compressor at high altitudes will be __________ as compared to that at sea level.

    • Options
    • A. same
    • B. lower
    • C. higher
    • Discuss
    • 5. In a turbo jet engine, subsequent to heat addition to compressed air, to get the power output, the working substance is expanded in

    • Options
    • A. exit nozzle, which is a constant volume process
    • B. exit nozzle, which is essentially an isentropic process
    • C. turbine blades, which is a constant volume process
    • D. turbine blades, which is essentially an isentropic process
    • Discuss
    • 6. Workdone by an air compressor __________ upon the way in which the air is compressed.

    • Options
    • A. depends
    • B. does not depend
    • Discuss
    • 7. A rocket engine uses __________ for the combustion of its fuel.

    • Options
    • A. surrounding air
    • B. compressed atmospheric air
    • C. its own oxygen
    • D. none of these
    • Discuss
    • 8. In jet propulsion power unit, the inlet duct of diverging shape is used for converting kinetic energy of air into pressure energy.

    • Options
    • A. True
    • B. False
    • Discuss
    • 9. The pressure ratio in a centrifugal compressor can be increased by increasing the tip speed and lowering the inlet temperature.

    • Options
    • A. Correct
    • B. Incorrect
    • Discuss
    • 10. A closed cycle gas turbine consists of a

    • Options
    • A. compressor
    • B. heating chamber
    • C. cooling chamber
    • D. all of these
    • Discuss


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