Blade passage flow structure effects on axial compressor rotating stall inception
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2005
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| Online Access: | http://hdl.handle.net/1721.1/10623 |
| _version_ | 1811096664969052160 |
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| author | Hoying, Donald Andrew |
| author2 | Edward M. Greitzer. |
| author_facet | Edward M. Greitzer. Hoying, Donald Andrew |
| author_sort | Hoying, Donald Andrew |
| collection | MIT |
| description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996. |
| first_indexed | 2024-09-23T16:47:05Z |
| format | Thesis |
| id | mit-1721.1/10623 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T16:47:05Z |
| publishDate | 2005 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/106232019-04-12T20:24:46Z Blade passage flow structure effects on axial compressor rotating stall inception Hoying, Donald Andrew Edward M. Greitzer. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics Aeronautics and Astronautics Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996. Includes bibliographical references (p. 125-130). by Donald Andrew Hoying. Ph.D. 2005-08-18T17:20:39Z 2005-08-18T17:20:39Z 1996 1996 Thesis http://hdl.handle.net/1721.1/10623 36266242 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 230 p. 13916825 bytes 13916580 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics Hoying, Donald Andrew Blade passage flow structure effects on axial compressor rotating stall inception |
| title | Blade passage flow structure effects on axial compressor rotating stall inception |
| title_full | Blade passage flow structure effects on axial compressor rotating stall inception |
| title_fullStr | Blade passage flow structure effects on axial compressor rotating stall inception |
| title_full_unstemmed | Blade passage flow structure effects on axial compressor rotating stall inception |
| title_short | Blade passage flow structure effects on axial compressor rotating stall inception |
| title_sort | blade passage flow structure effects on axial compressor rotating stall inception |
| topic | Aeronautics and Astronautics |
| url | http://hdl.handle.net/1721.1/10623 |
| work_keys_str_mv | AT hoyingdonaldandrew bladepassageflowstructureeffectsonaxialcompressorrotatingstallinception |