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The effect of the boundary layer upon the flow in a conical hypersonic wind tunnel nozzle

dc.contributor.authorSichel, Martinen_US
dc.date.accessioned2006-02-03T17:45:29Z
dc.date.available2006-02-03T17:45:29Z
dc.date.issued1963en_US
dc.identifierUMR3599en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/7595
dc.format.extent84 bytes
dc.format.extent89170 bytes
dc.format.extent3366 bytes
dc.format.extent111978 bytes
dc.format.extent5646894 bytes
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.subjectAerodynamics, Hypersonic.en_US
dc.subjectHypersonic Wind Tunnels.en_US
dc.subjectBoundary Layer.en_US
dc.titleThe effect of the boundary layer upon the flow in a conical hypersonic wind tunnel nozzleen_US
dc.typeTechnical Reporten_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/7595/5/bad2101.0001.001.pdfen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/7595/4/bad2101.0001.001.txten_US
dc.owningcollnameEngineering, College of - Technical Reports


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