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Shock waves in transonic channel flows at moderate Reynolds number
dc.contributor.authorMace, J. L.en_US
dc.contributor.authorAdamson, Thomas Charles Jr.en_US
dc.date.accessioned2010-06-11T18:04:52Z
dc.date.available2010-06-11T18:04:52Z
dc.date.issued1985en_US
dc.identifier.citationMace, J.; Adamson, T. C., Jr. (1985). "Shock waves in transonic channel flows at moderate Reynolds number" AIAA-1985-369, American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting, 23rd, Reno, NV, Jan 14-17, 1985. 11 p.. <http://hdl.handle.net/2027.42/76259>en_US
dc.identifier.otherAIAA-1985-369en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76259
dc.format.extent670003 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleShock waves in transonic channel flows at moderate Reynolds numberen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumMichigan, University, Ann Arbor, MIen_US
dc.contributor.affiliationotherUSAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OHen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76259/1/AIAA-1985-369-965.pdf
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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