A numerical model for supersonic reacting mixing layers
A current research effort is underway at the NASA Langley Research Center to achieve a detailed understanding of important phenomena present when a supersonic flow undergoes a chemical reaction. A computer program has been developed to study the details of such flows. The program has been constructe...
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Veröffentlicht in: | Computer methods in applied mechanics and engineering 1987-10, Vol.64 (1), p.39-60 |
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creator | Philip Drummond, J. Clayton Rogers, R. Yousuff Hussaini, M. |
description | A current research effort is underway at the NASA Langley Research Center to achieve a detailed understanding of important phenomena present when a supersonic flow undergoes a chemical reaction. A computer program has been developed to study the details of such flows. The program has been constructed to consider the multicomponent diffusion and convection of important species, the finite-rate reaction of these species, and the resulting interaction between the fluid mechanics and chemistry. Code results from the analysis of a spatially developing and reacting mixing layer are presented, and conclusions are drawn regarding the structure of the evolving layer and its associated flame. |
doi_str_mv | 10.1016/0045-7825(87)90032-6 |
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Code results from the analysis of a spatially developing and reacting mixing layer are presented, and conclusions are drawn regarding the structure of the evolving layer and its associated flame.</description><subject>Compressible flows; shock and detonation phenomena</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fluid Mechanics And Heat Transfer</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><issn>0045-7825</issn><issn>1879-2138</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1987</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNp9kE1LxDAQhoMouK7-gz30IKKH6iRpmvQiLItfsOBFzyGbTiTSjzVpxf33tnbZo3OZw_u8w_AQsqBwS4HmdwCZSKVi4lrJmwKAszQ_IjOqZJEyytUxmR2QU3IW4ycMoyibEblMmr7G4K2pkrotsUpcG5LYbzHEtvE2CWhs55uPpPY_46rMbojOyYkzVcSL_Z6T98eHt9Vzun59elkt16nlSnSpcFJyJksDmBvDGbUqMyAdFbSwZVk6zh23GwVqY2BjVUkNOuZyCQyts5TPydV0dxvarx5jp2sfLVaVabDto2aZEFLJfACzCbShjTGg09vgaxN2moIeLelRgR4VaCX1nyU91i73900cFLhgGuvjoStzQYWAAVtMWGOi0U0XoqaFUgACKJNDfD_FOKj49hh0tB4bi6UPaDtdtv7_N34BxGqDug</recordid><startdate>19871001</startdate><enddate>19871001</enddate><creator>Philip Drummond, J.</creator><creator>Clayton Rogers, R.</creator><creator>Yousuff Hussaini, M.</creator><general>Elsevier B.V</general><general>Elsevier</general><scope>CYE</scope><scope>CYI</scope><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope></search><sort><creationdate>19871001</creationdate><title>A numerical model for supersonic reacting mixing layers</title><author>Philip Drummond, J. ; Clayton Rogers, R. ; Yousuff Hussaini, M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c385t-5f77327da0e6aa321c84a07f1519cdddf33f3cb808ba0bc8d1aef2f6702ecfc13</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1987</creationdate><topic>Compressible flows; shock and detonation phenomena</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fluid Mechanics And Heat Transfer</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Philip Drummond, J.</creatorcontrib><creatorcontrib>Clayton Rogers, R.</creatorcontrib><creatorcontrib>Yousuff Hussaini, M.</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Computer methods in applied mechanics and engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Philip Drummond, J.</au><au>Clayton Rogers, R.</au><au>Yousuff Hussaini, M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A numerical model for supersonic reacting mixing layers</atitle><jtitle>Computer methods in applied mechanics and engineering</jtitle><date>1987-10-01</date><risdate>1987</risdate><volume>64</volume><issue>1</issue><spage>39</spage><epage>60</epage><pages>39-60</pages><issn>0045-7825</issn><eissn>1879-2138</eissn><coden>CMMECC</coden><abstract>A current research effort is underway at the NASA Langley Research Center to achieve a detailed understanding of important phenomena present when a supersonic flow undergoes a chemical reaction. 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source | Elsevier ScienceDirect Journals; NASA Technical Reports Server |
subjects | Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fluid Mechanics And Heat Transfer Fundamental areas of phenomenology (including applications) Physics |
title | A numerical model for supersonic reacting mixing layers |
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