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Mixing Effectiveness Study in Scramjet Combustion

dc.citation.epage229en_US
dc.citation.spage218en_US
dc.citation.volume67en_US
dc.citation.woscount0en_US
dc.contributor.authorChen, Y. S.en_US
dc.contributor.authorLian, Y. Y.en_US
dc.contributor.authorChou, T. H.en_US
dc.contributor.authorLai, Alfreden_US
dc.contributor.authorWu, J. S.en_US
dc.contributor.department交大名義發表zh_TW
dc.contributor.departmentNational Chiao Tung Universityen_US
dc.date.accessioned2019-04-03T06:47:39Z
dc.date.available2019-04-03T06:47:39Z
dc.date.issued2013-01-01en_US
dc.description.abstractScramjet propulsion provides promising opportunities for high-speed transportation and cost reduction for satellite and spacecraft launch operations. This paper provides some selected numerical examples among the abundance of available test cases for the purpose of demonstrating to what extends the current computational models can do in assisting the design and test programs of scramjet combustors. Numerical examples that cover a wide range of flight speeds are investigated with benchmark data validations. Ideas of mixing enhancement and flame holding mechanisms in scramjet combustion is analyzed and planned for the future experimental investigations. (C) 2013 The Authors. Published by Elsevier Ltd.en_US
dc.identifier.doi10.1016/j.proeng.2013.12.021en_US
dc.identifier.issn1877-7058en_US
dc.identifier.journal7TH ASIAN-PACIFIC CONFERENCE ON AEROSPACE TECHNOLOGY AND SCIENCE, APCATS 2013en_US
dc.identifier.urihttp://dx.doi.org/10.1016/j.proeng.2013.12.021en_US
dc.identifier.urihttps://ir.lib.nycu.edu.tw/handle/11536/135391
dc.identifier.wosnumberWOS:000333561700021en_US
dc.language.isoen_USen_US
dc.subjectScarmjeten_US
dc.subjectComputational Fluid Dynamicsen_US
dc.subjectFinite-rate Chemistryen_US
dc.subjectFuel Injectionen_US
dc.subjectMixing Enhancementen_US
dc.titleMixing Effectiveness Study in Scramjet Combustionen_US
dc.typeProceedings Paperen_US

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