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dc.contributor.authorGiles, M. (Michael)en_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratory.en_US
dc.date.accessioned2005-08-10T23:43:22Z
dc.date.available2005-08-10T23:43:22Z
dc.date.issued1985en_US
dc.identifier.otherno. 186en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/13815
dc.descriptionThesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1985.en_US
dc.description"October 1985."en_US
dc.descriptionIncludes bibliographical references (p. 167-169).en_US
dc.description.sponsorshipResearch sponsored by the Air Force Office of Scientific Research. F49620-78-C-0084en_US
dc.description.statementofresponsibilityby Michael B. Giles.en_US
dc.format.extent170 p.en_US
dc.format.extent13518363 bytes
dc.format.extent13518116 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoengen_US
dc.publisherGas Turbine Laboratory, Massachusetts Institute of Technologyen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.relation.ispartofseriesGTL report ; #186.en_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/1721.1/7582
dc.subjectGas Turbine Laboratory.en_US
dc.subject.lccTJ778.M41 G24 no.186en_US
dc.titleNewton solution of steady two-dimensional transonic flowen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc24566081en_US


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