Compressors, Gas Dynamics and Gas Turbines - Data Intensity 2 Multiple Questions and Answers.
Exercise Questions ::
Compressors, Gas Dynamics and Gas Turbines
11. | In axial flow compressor, exit flow angle deviation from the blade angle is a function of |
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| A. | blade camber |
| B. | blade camber and incidence angle |
| C. | space-chord ratio |
| D. | blade camber and space-chord ratio |
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Published by:Michael Daani
12. | Rotary compressors are used for delivering |
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| A. | small quantities of air at high pressures |
| B. | large quantities of air at high pressures |
| C. | small quantities of air at low pressures |
| D. | large quantities of air at low pressures |
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Published by:Michael Daani
Published by:Michael Daani
14. | In a centrifugal compressor, an increase in speed at a given pressure ratio causes |
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| A. | increase in flow |
| B. | decrease in flow |
| C. | increase in efficiency |
| D. | increase in flow and decrease in efficiency |
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Published by:Michael Daani
15. | A large clearance Volume in a reciprocating compressor results in |
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| A. | reduced volume flow rate |
| B. | increased volume flow rate |
| C. | lower suction pressure |
| D. | lower delivery pressure |
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Published by:Michael Daani
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