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dc.contributor.advisorChoon S. Tan.en_US
dc.contributor.authorStanislaw, Gregory Scotten_US
dc.date.accessioned2009-12-10T18:54:21Z
dc.date.available2009-12-10T18:54:21Z
dc.date.copyright1997en_US
dc.date.issued1997en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/49969
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.en_US
dc.descriptionIncludes bibliographical references (p. 78-80).en_US
dc.description.statementofresponsibilityby Gregory Scott Stanislaw.en_US
dc.format.extent102 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 Astronauticsen_US
dc.titleUtility of the flow substitution principle for high speed propulsion applicationsen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc36829827en_US


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