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Effect of the boundary layer upon the flow in a conical hypersonic nozzle
dc.contributor.authorSichel, Martinen_US
dc.date.accessioned2010-06-11T18:29:58Z
dc.date.available2010-06-11T18:29:58Z
dc.date.issued1964en_US
dc.identifier.citationSichel, M. (1964). "Effect of the boundary layer upon the flow in a conical hypersonic nozzle" AIAA Journal, vol.2 no.1 (180-183). <http://hdl.handle.net/2027.42/76641>en_US
dc.identifier.issn0001-1452en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76641
dc.format.extent581468 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleEffect of the boundary layer upon the flow in a conical hypersonic nozzleen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumMICHIGAN, U., DEPT. OF AERONAUTICAL AND ASTRONAUTICAL ENGINEERING, ANN ARBOR, MICH.en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76641/1/AIAA-2269-288.pdf
dc.identifier.doi10.2514/3.2269en_US
dc.identifier.sourceAIAA Journalen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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