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An axisymmetric similarity solution for viscous transonic nozzle flow

dc.contributor.authorSichel, Martinen_US
dc.contributor.authorYin, Yung-Kohen_US
dc.date.accessioned2006-02-03T18:30:36Z
dc.date.available2006-02-03T18:30:36Z
dc.date.issued1966en_US
dc.identifierUMR3597en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/7598
dc.format.extent29 bytes
dc.format.extent22666 bytes
dc.format.extent3366 bytes
dc.format.extent28676 bytes
dc.format.extent1355777 bytes
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
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dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.subjectAerodynamics, Transonic -- Mathematical Models.en_US
dc.subjectShock Waves.en_US
dc.titleAn axisymmetric similarity solution for viscous transonic nozzle flowen_US
dc.typeTechnical Reporten_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/7598/5/bad2096.0001.001.pdfen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/7598/4/bad2096.0001.001.txten_US
dc.owningcollnameEngineering, College of - Technical Reports


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