Discussion
Home ‣ Mechanical Engineering ‣ Compressors, Gas Dynamics and Gas Turbines Comments
- Question
When the temperature of air leaving the intercooler, in a two stage compression with intercooler, is __________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.
Options- A. equal to
- B. less than
- C. more than
- Correct Answer
- equal to
- 1. The clearance volume in the compressor is kept minimum because it effects on volumetric efficiency.
Options- A. Correct
- B. Incorrect Discuss
- 2. Which of the following statement is correct?
Options- A. The ratio of the discharge pressure to the inlet pressure of air is called compressor efficiency.
- B. The compression ratio for the compressor is always greater than unity.
- C. The compressor capacity is the ratio of workdone per cycle to the stroke volume.
- D. During isothermal compression of air, the workdone in a compressor is maximum. Discuss
- 3. The ratio of workdone per cycle to the stroke volume of the compressor is known as
Options- A. compressor capacity
- B. compression ratio
- C. compressor efficiency
- D. mean effective pressure Discuss
- 4. The compressed air may be used
Options- A. in gas turbine plants
- B. for operating pneumatic drills
- C. in starting and supercharging of I.C. engines
- D. all of the above Discuss
- 5. The volume of air delivered by the compressor is called
Options- A. free air delivery
- B. compressor capacity
- C. swept volume
- D. none of these Discuss
- 6. The increase in pressure in a vane blower takes place first due to compression and then due to back flow of air.
Options- A. Correct
- B. Incorrect Discuss
- 7. Intercooling in multi-stage compressors is done
Options- A. to cool the air during compression
- B. to cool the air at delivery
- C. to enable compression in two stages
- D. to minimise the work of compression Discuss
- 8. The stagnation pressure rise in a centrifugal compressor takes place
Options- A. in the diffuser only
- B. in the impeller only
- C. in the diffuser and impeller
- D. in the inlet guide vanes only Discuss
- 9. The type of rotary compressor used in aeroplanes, is of
Options- A. centrifugal type
- B. axial flow type
- C. radial flow type
- D. none of these Discuss
- 10. In a centrifugal compressor, an increase in speed at a given pressure ratio causes
Options- A. increase in flow
- B. decrease in flow
- C. increase in efficiency
- D. increase in flow and decrease in efficiency Discuss
Compressors, Gas Dynamics and Gas Turbines problems
Search Results
Correct Answer: Correct
Correct Answer: The compression ratio for the compressor is always greater than unity.
Correct Answer: mean effective pressure
Correct Answer: all of the above
Correct Answer: compressor capacity
Correct Answer: Correct
Correct Answer: to minimise the work of compression
Correct Answer: in the diffuser and impeller
Correct Answer: axial flow type
Correct Answer: increase in flow and decrease in efficiency
Comments
There are no comments.More in Mechanical Engineering:
Programming
Copyright ©CuriousTab. All rights reserved.