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dc.contributor.advisorJames D. Paduano.en_US
dc.contributor.authorLuers, Andrew Scott, 1978-en_US
dc.contributor.otherMassachusetts Institute of Technology. Technology and Policy Program.en_US
dc.date.accessioned2013-12-06T20:41:32Z
dc.date.available2013-12-06T20:41:32Z
dc.date.copyright2003en_US
dc.date.issued2003en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/82780
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (S.M.)--Massachusetts Institute of Technology, Engineering Systems Division, Technology and Policy Program, 2003.en_US
dc.descriptionIncludes bibliographical references (p. 177-181).en_US
dc.description.statementofresponsibilityby Andrew Scott Luers.en_US
dc.format.extent181 p.en_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.subjectTechnology and Policy Program.en_US
dc.titleFlow control techniques in a serpentine inlet : an enabling technology to increase the military viability of unmanned air vehiclesen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.contributor.departmentMassachusetts Institute of Technology. Engineering Systems Division
dc.contributor.departmentTechnology and Policy Program
dc.identifier.oclc54090379en_US


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