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Numerical Investigation of Shock-Train Response to Inflow Boundary-Layer Variations

dc.contributor.authorFiévet, Romain
dc.contributor.authorKoo, Heeseok
dc.contributor.authorRaman, Venkat
dc.contributor.authorAuslender, Aaron H.
dc.date.accessioned2018-04-11T19:04:59Z
dc.date.available2018-04-11T19:04:59Z
dc.date.issued2017
dc.identifier.citationFiévet, Romain; Koo, Heeseok; Raman, Venkat; Auslender, Aaron H. (2017). "Numerical Investigation of Shock-Train Response to Inflow Boundary-Layer Variations." AIAA Journal, 55(9), 2888-2901.
dc.identifier.issn0001-1452
dc.identifier.urihttps://hdl.handle.net/2027.42/143113
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.titleNumerical Investigation of Shock-Train Response to Inflow Boundary-Layer Variations
dc.typeArticle
dc.subject.hlbsecondlevelAerospace Engineering
dc.subject.hlbtoplevelEngineering
dc.description.peerreviewedPeer Reviewed
dc.description.bitstreamurlhttps://deepblue.lib.umich.edu/bitstream/2027.42/143113/1/1.J055333.pdf
dc.identifier.doi10.2514/1.J055333
dc.identifier.sourceAIAA Journal
dc.owningcollnameAerospace Engineering, Department of


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