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dc.contributor.advisorMark Drela.en_US
dc.contributor.authorCali, Philip Marken_US
dc.date.accessioned2008-11-07T19:22:34Z
dc.date.available2008-11-07T19:22:34Z
dc.date.copyright1992en_US
dc.date.issued1992en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/43266
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.en_US
dc.descriptionIncludes bibliographical references (leaves 61-62).en_US
dc.description.statementofresponsibilityby Philip Mark Cali.en_US
dc.format.extent62 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.titleImplicit Euler calculation of supersonic vortex wake/engine plume interactionen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc27995189en_US


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