No AccessNumerical simulation on detonation initiation and propagation in supersonic combustible mixtures with nonuniform speciesXiaodong Cai, Jianhan Liang and Zhiyong LinXiaodong CaiHypersonic Propulsion CenterSearch for more papers by this author, Jianhan LiangHypersonic Propulsion CenterSearch for more papers by this author and Zhiyong LinHypersonic Propulsion CenterSearch for more papers by this authorAIAA 2015-3527Session: Hypersonic Fundamentals IVPublished Online:2 Jul 2015https://doi.org/10.2514/6.2015-3527SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byDetonation Interaction with Boundary Layer in Supersonic Combustible MixtureWeiqiang Chen, Jianhan Liang, Xiaodong Cai and Zhiyong Lin2 March 2017 What's Popular 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 6-9 July 2015Glasgow, Scotlandhttps://doi.org/10.2514/6.2015-3527 CrossmarkInformationCopyright © 2015 by The Aerospace Corporation. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAerospace SciencesComputational Fluid DynamicsEquations of Fluid DynamicsFinite Volume MethodFluid DynamicsNormal Shock WaveNumerical AnalysisOblique Shock WaveShock WavesVortex Dynamics KeywordsDeflagration to Detonation TransitionTotal Variation DiminishingDetonation WavesStructured Adaptive Mesh RefinementVorticesOblique Shock WaveMach ReflectionScramjetRankine Hugoniot EquationsFinite Volume MethodDigital Topics