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dc.contributor.advisorCharles Boppe and Zoltan S. Spakovszky.en_US
dc.contributor.authorHanlon, Christopher J. (Christopher Joseph), 1978-en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2013-12-06T20:39:14Z
dc.date.available2013-12-06T20:39:14Z
dc.date.copyright2003en_US
dc.date.issued2003en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/82759
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.en_US
dc.descriptionIncludes bibliographical references (leaf 91).en_US
dc.description.statementofresponsibilityby Christopher J. Hanlon.en_US
dc.format.extent94 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 Astronautics.en_US
dc.titleEngine design implications for a blended wing-body aircraft with boundary later ingestionen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc54069199en_US


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