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The experimental and theoretical pressure distribution and normal force of a cone-cylinder configuration at a Mach number of 1.93

dc.contributor.authorDorrance, William H.en_US
dc.contributor.authorRoss, F. W.en_US
dc.date.accessioned2006-02-03T16:58:53Z
dc.date.available2006-02-03T16:58:53Z
dc.date.issued1949en_US
dc.identifierUMR4167en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/4636
dc.format.extent28 bytes
dc.format.extent76338 bytes
dc.format.extent3366 bytes
dc.format.extent93959 bytes
dc.format.extent6115315 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, Supersonic.en_US
dc.subjectSupersonic wind tunnels.en_US
dc.titleThe experimental and theoretical pressure distribution and normal force of a cone-cylinder configuration at a Mach number of 1.93en_US
dc.typeTechnical Reporten_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/4636/5/bad5605.0001.001.pdfen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/4636/4/bad5605.0001.001.txten_US
dc.owningcollnameEngineering, College of - Technical Reports


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