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Compressors, Gas Dynamics and Gas Turbines problems


  • 1. The ratio of the discharge pressure to the inlet pressure of air is called

  • Options
  • A. compression ratio
  • B. expansion ratio
  • C. compressor efficiency
  • D. volumetric efficiency
  • Discuss
  • 2. Which of the following bladings will give maximum pressure rise in a centrifugal compressor, assuming the same overall dimensions, blade inlet angle and rotational speeds?

  • Options
  • A. Forward curved blades
  • B. Backward curved blades
  • C. Radial blades
  • D. all of these
  • Discuss
  • 3. In an axial flow compressor, the ratio of pressure in theTOtor blades to the pressure rise in the compressor in one stage is known as

  • Options
  • A. work factor
  • B. slip factor
  • C. degree of reaction
  • D. pressure coefficient
  • Discuss
  • 4. In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

  • Options
  • A. atmosphere
  • B. vacuum
  • C. discharge nozzle
  • D. back to the compressor
  • Discuss
  • 5. Reheating in a multi-stage expansion gas turbine __________ compressor work.

  • Options
  • A. has no effect on
  • B. decreases
  • C. increases
  • Discuss
  • 6. The volumetric efficiency of a compressor

  • Options
  • A. increases with decrease in compression ratio
  • B. decreases with decrease in compression ratio
  • C. increases with increase in compression ratio
  • D. decreases with increase in compression ratio
  • Discuss
  • 7. The volume of air sucked by the compressor during its suction stroke is called

  • Options
  • A. free air delivery
  • B. compressor capacity
  • C. swept volume
  • D. none of these
  • Discuss
  • 8. A compressor mostly used for supercharging of I.C. engines is

  • Options
  • A. radial flow compressor
  • B. axial flow compressor
  • C. roots blower
  • D. reciprocating compressor
  • Discuss
  • 9. The free air delivery is the volume of air that can be delivered by a compressor freely.

  • Options
  • A. True
  • B. False
  • Discuss
  • 10. A regenerator in a gas turbine improves thermal efficiency.

  • Options
  • A. Correct
  • B. Incorrect
  • Discuss

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