Detonation waves induced by a confined wedge
An auto-ignition detonation phenomenon can be initiated by a wedge confined in a channel. A new, self-sustaining, normal detonation wave engine concept is proposed. The detonation processes were numerically modeled with a simplified two-dimensional wedged channel flow that was deemed to emulate a re...
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Veröffentlicht in: | Aerospace science and technology 2006-12, Vol.10 (8), p.679-685 |
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creator | Lu, Frank K. Fan, Huiyuan Wilson, Donald R. |
description | An auto-ignition detonation phenomenon can be initiated by a wedge confined in a channel. A new, self-sustaining, normal detonation wave engine concept is proposed. The detonation processes were numerically modeled with a simplified two-dimensional wedged channel flow that was deemed to emulate a real three-dimensional configuration. The results showed that within certain ranges of incoming flow Mach number or wedge angle, detonation could be self ignited in the channel. The study furthermore investigated the detonation waves based on three different detonation initiation positions. Different configurations of the detonation waves were observed and analyzed. The performance of the different detonation wave configurations was estimated and compared. |
doi_str_mv | 10.1016/j.ast.2006.06.005 |
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A new, self-sustaining, normal detonation wave engine concept is proposed. The detonation processes were numerically modeled with a simplified two-dimensional wedged channel flow that was deemed to emulate a real three-dimensional configuration. The results showed that within certain ranges of incoming flow Mach number or wedge angle, detonation could be self ignited in the channel. The study furthermore investigated the detonation waves based on three different detonation initiation positions. Different configurations of the detonation waves were observed and analyzed. The performance of the different detonation wave configurations was estimated and compared.</description><identifier>ISSN: 1270-9638</identifier><identifier>EISSN: 1626-3219</identifier><identifier>DOI: 10.1016/j.ast.2006.06.005</identifier><language>eng</language><publisher>Paris: Elsevier SAS</publisher><subject>Compressible flows; shock and detonation phenomena ; Detonation ; Exact sciences and technology ; Fluid dynamics ; Fundamental areas of phenomenology (including applications) ; Physics ; Propulsion system ; Shock ; Shock-wave interactions and shock effects ; Shock-wave interactions and shockeffects ; Wave propagation</subject><ispartof>Aerospace science and technology, 2006-12, Vol.10 (8), p.679-685</ispartof><rights>2006 Elsevier SAS</rights><rights>2007 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c358t-679ce4c37a452cf376508867ebba49dcdbbbdc59709dceaf0d54db2ff546f4f53</citedby><cites>FETCH-LOGICAL-c358t-679ce4c37a452cf376508867ebba49dcdbbbdc59709dceaf0d54db2ff546f4f53</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S1270963806000794$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=18337379$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Lu, Frank K.</creatorcontrib><creatorcontrib>Fan, Huiyuan</creatorcontrib><creatorcontrib>Wilson, Donald R.</creatorcontrib><title>Detonation waves induced by a confined wedge</title><title>Aerospace science and technology</title><description>An auto-ignition detonation phenomenon can be initiated by a wedge confined in a channel. A new, self-sustaining, normal detonation wave engine concept is proposed. The detonation processes were numerically modeled with a simplified two-dimensional wedged channel flow that was deemed to emulate a real three-dimensional configuration. The results showed that within certain ranges of incoming flow Mach number or wedge angle, detonation could be self ignited in the channel. The study furthermore investigated the detonation waves based on three different detonation initiation positions. Different configurations of the detonation waves were observed and analyzed. The performance of the different detonation wave configurations was estimated and compared.</description><subject>Compressible flows; shock and detonation phenomena</subject><subject>Detonation</subject><subject>Exact sciences and technology</subject><subject>Fluid dynamics</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Physics</subject><subject>Propulsion system</subject><subject>Shock</subject><subject>Shock-wave interactions and shock effects</subject><subject>Shock-wave interactions and shockeffects</subject><subject>Wave propagation</subject><issn>1270-9638</issn><issn>1626-3219</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2006</creationdate><recordtype>article</recordtype><recordid>eNp9UE1LAzEUDKJgrf4Ab3vRk7vmY5Ps4knqJxS86DlkkxdJabM12bb035ulBW_CwHsD8-Yxg9A1wRXBRNwvKp2GimIsqhGYn6AJEVSUjJL2NO9U4rIVrDlHFyktMMa0rekE3T3B0Ac9-D4UO72FVPhgNwZs0e0LXZg-OB8y24H9hkt05vQywdVxTtHXy_Pn7K2cf7y-zx7npWG8GUohWwO1YVLXnBrHpOC4aYSErtN1a43tus4a3kqcCWiHLa9tR53jtXC142yKbg--69j_bCANauWTgeVSB-g3SdE2hyKszUJyEJrYpxTBqXX0Kx33imA19qIWKveixl7UCDya3xzNdTJ66aIOxqe_w4YxyeTo_XDQQU669RBVMh5CrsZHMIOyvf_nyy-O63fX</recordid><startdate>20061201</startdate><enddate>20061201</enddate><creator>Lu, Frank K.</creator><creator>Fan, Huiyuan</creator><creator>Wilson, Donald R.</creator><general>Elsevier SAS</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20061201</creationdate><title>Detonation waves induced by a confined wedge</title><author>Lu, Frank K. ; Fan, Huiyuan ; Wilson, Donald R.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c358t-679ce4c37a452cf376508867ebba49dcdbbbdc59709dceaf0d54db2ff546f4f53</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2006</creationdate><topic>Compressible flows; shock and detonation phenomena</topic><topic>Detonation</topic><topic>Exact sciences and technology</topic><topic>Fluid dynamics</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Physics</topic><topic>Propulsion system</topic><topic>Shock</topic><topic>Shock-wave interactions and shock effects</topic><topic>Shock-wave interactions and shockeffects</topic><topic>Wave propagation</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Lu, Frank K.</creatorcontrib><creatorcontrib>Fan, Huiyuan</creatorcontrib><creatorcontrib>Wilson, Donald R.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Aerospace science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Lu, Frank K.</au><au>Fan, Huiyuan</au><au>Wilson, Donald R.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Detonation waves induced by a confined wedge</atitle><jtitle>Aerospace science and technology</jtitle><date>2006-12-01</date><risdate>2006</risdate><volume>10</volume><issue>8</issue><spage>679</spage><epage>685</epage><pages>679-685</pages><issn>1270-9638</issn><eissn>1626-3219</eissn><abstract>An auto-ignition detonation phenomenon can be initiated by a wedge confined in a channel. A new, self-sustaining, normal detonation wave engine concept is proposed. The detonation processes were numerically modeled with a simplified two-dimensional wedged channel flow that was deemed to emulate a real three-dimensional configuration. The results showed that within certain ranges of incoming flow Mach number or wedge angle, detonation could be self ignited in the channel. The study furthermore investigated the detonation waves based on three different detonation initiation positions. Different configurations of the detonation waves were observed and analyzed. The performance of the different detonation wave configurations was estimated and compared.</abstract><cop>Paris</cop><pub>Elsevier SAS</pub><doi>10.1016/j.ast.2006.06.005</doi><tpages>7</tpages></addata></record> |
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subjects | Compressible flows shock and detonation phenomena Detonation Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Propulsion system Shock Shock-wave interactions and shock effects Shock-wave interactions and shockeffects Wave propagation |
title | Detonation waves induced by a confined wedge |
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