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Effects of continuum breakdown on hypersonic aerothermodynamics for reacting flow
dc.contributor.authorHolman, Timothy D.en_US
dc.contributor.authorBoyd, Iain D.en_US
dc.date.accessioned2013-07-03T19:31:47Z
dc.date.available2013-07-03T19:31:47Z
dc.date.issued2011-02en_US
dc.identifier.citationHolman, Timothy D.; Boyd, Iain D. (2011). "Effects of continuum breakdown on hypersonic aerothermodynamics for reacting flow." Physics of Fluids, 23(2): 27101. <http://hdl.handle.net/2027.42/98744>en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/98744
dc.publisherThe American Institute of Physicsen_US
dc.subjectAerodynamicsen_US
dc.subjectAircraften_US
dc.subjectComputational Fluid Dynamicsen_US
dc.subjectFlow Simulationen_US
dc.subjectHeat Transferen_US
dc.subjectHypersonic Flowen_US
dc.subjectKnudsen Flowen_US
dc.subjectMach Numberen_US
dc.subjectMonte Carlo Methodsen_US
dc.titleEffects of continuum breakdown on hypersonic aerothermodynamics for reacting flowen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/98744/1/PhysFluids_23_027101.pdf
dc.identifier.doi10.1063/1.3541816en_US
dc.identifier.sourcePhysics of Fluidsen_US
dc.owningcollnamePhysics, Department of


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