| dc.contributor.advisor | Michael B. Giles. | en_US |
| dc.contributor.author | Lindquist, Dana Rae | en_US |
| dc.date.accessioned | 2005-08-15T16:05:50Z | |
| dc.date.available | 2005-08-15T16:05:50Z | |
| dc.date.copyright | 1992 | en_US |
| dc.date.issued | 1992 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/13090 | |
| dc.description | Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992. | en_US |
| dc.description | Includes bibliographical references (leaves 190-192). | en_US |
| dc.description.statementofresponsibility | by Dana Rae Lindquist. | en_US |
| dc.format.extent | 206 leaves | en_US |
| dc.format.extent | 10288326 bytes | |
| dc.format.extent | 10288083 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.format.mimetype | application/pdf | |
| 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 | Computation of unsteady transonic flowfields using shock capturing and the linear perturbation Euler equations | en_US |
| dc.type | Thesis | en_US |
| dc.description.degree | Ph.D. | en_US |
| dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | |
| dc.identifier.oclc | 26368644 | en_US |
