Citation
Williams, Allen Dean (1960) The Effect of Tip Clearance Flows on Performance of Axial Flow Compressors. Engineer's thesis, California Institute of Technology. doi:10.7907/7T14-SP07. https://resolver.caltech.edu/CaltechETD:etd-12092005-163445
Abstract
The change in rotor performance with tip clearance of an axial flow compressor over a wide range of flow rates above stall was investigated to gain more understanding of the effect of the tip flow mechanism on rotor performance. The experimental results were compared with a flow model proposed previously and found to be in reasonable agreement.
Item Type: | Thesis (Engineer's thesis) |
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Subject Keywords: | (Aeronautical Engineering) |
Degree Grantor: | California Institute of Technology |
Division: | Engineering and Applied Science |
Major Option: | Aeronautics |
Thesis Availability: | Public (worldwide access) |
Research Advisor(s): |
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Group: | GALCIT |
Thesis Committee: |
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Defense Date: | 1 January 1960 |
Record Number: | CaltechETD:etd-12092005-163445 |
Persistent URL: | https://resolver.caltech.edu/CaltechETD:etd-12092005-163445 |
DOI: | 10.7907/7T14-SP07 |
Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
ID Code: | 4908 |
Collection: | CaltechTHESIS |
Deposited By: | Imported from ETD-db |
Deposited On: | 12 Dec 2005 |
Last Modified: | 09 Nov 2023 00:58 |
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