| dc.contributor.author | Schulmeyer, Andreas | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. | en_US |
| dc.date.accessioned | 2008-02-04T20:51:00Z | |
| dc.date.available | 2008-02-04T20:51:00Z | |
| dc.date.copyright | 1989 | en_US |
| dc.date.issued | 1989 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/40144 | |
| dc.description | Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989. | en_US |
| dc.description | GRSN 406823 | en_US |
| dc.description | Includes bibliographical references (leaf 37). | en_US |
| dc.description.statementofresponsibility | by Andreas Schulmeyer. | en_US |
| dc.format.extent | 82 leaves | en_US |
| dc.language.iso | eng | en_US |
| dc.publisher | Massachusetts Institute of Technology | en_US |
| dc.rights | 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. | en_US |
| dc.rights.uri | http://dspace.mit.edu/handle/1721.1/7582 | |
| dc.subject | Aeronautics and Astronautics. | en_US |
| dc.title | Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | M.S. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 22140692 | en_US |
