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dc.contributor.advisorEarll M. Murman, Mårten Landahl.en_US
dc.contributor.authorModiano, Daviden_US
dc.date.accessioned2009-12-10T18:44:41Z
dc.date.available2009-12-10T18:44:41Z
dc.date.copyright1993en_US
dc.date.issued1993en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/49895
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.en_US
dc.descriptionIncludes bibliographical references (leaves 139-146).en_US
dc.description.statementofresponsibilityby David Laurence Modiano.en_US
dc.format.extent146 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.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.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleAdaptive mesh Euler equation computation of vortex breakdown in delta wing flowen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc28141922en_US


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