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A physical description of a variable-Mach-number 4- by 4-inch pilot corner nozzle
dc.contributor.authorLiepman, Hans Peteren_US
dc.contributor.authorMurphy, J. S.en_US
dc.contributor.authorNourse, J. H.en_US
dc.date.accessioned2006-02-03T17:06:22Z
dc.date.available2006-02-03T17:06:22Z
dc.date.issued1953en_US
dc.identifierUMR3011en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/6304
dc.format.extent20 bytes
dc.format.extent23642 bytes
dc.format.extent3366 bytes
dc.format.extent29443 bytes
dc.format.extent4426242 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.subjectSupersonic nozzles -- Design and construction.en_US
dc.subjectSupersonic wind tunnels.en_US
dc.titleA physical description of a variable-Mach-number 4- by 4-inch pilot corner nozzleen_US
dc.typeTechnical Reporten_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/6304/5/bad0308.0001.001.pdfen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/6304/4/bad0308.0001.001.txten_US
dc.owningcollnameEngineering, College of - Technical Reports


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