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Adaptive Turbulent Schmidt number approach for Multi-Scale Simulation of Supersonic Crossflow
dc.contributor.authorHassan, Ezeldinen_US
dc.contributor.authorAono, Hikaruen_US
dc.contributor.authorShyy, Weien_US
dc.contributor.authorBoles, Johnen_US
dc.contributor.authorDavis, Douglasen_US
dc.date.accessioned2012-04-05T20:37:07Z
dc.date.available2012-04-05T20:37:07Z
dc.date.issued2011en_US
dc.identifier.citationHassan, Ezeldin; Aono, Hikaru; Shyy, Wei; Boles, John; Davis, Douglas (2011). "Adaptive Turbulent Schmidt number approach for Multi-Scale Simulation of Supersonic Crossflow." 20th AIAA Computational Fluid Dynamics Conference, Honolulu, Hawaii, June 27-30, 2011, AIAA-2011-3702. <http://hdl.handle.net/2027.42/90695>en_US
dc.identifier.otherAIAA-2011-3702en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/90695
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleAdaptive Turbulent Schmidt number approach for Multi-Scale Simulation of Supersonic Crossflowen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationotherUniversity of Michigan, Ann Arbor, Ann Arbor, MI; University of Michigan, Ann Arbor, Ann Arbor, MI; Hong Kong University of Science and Technology, Kowloon, HONG KONG; Taitech, Inc., Beavercreek, OH; Air Force Research Laboratory, Fairborn, OHen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/90695/1/AIAA-2011-3702-910.pdf
dc.owningcollnameAerospace Engineering, Department of


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