The influence of acoustic impedance on gaseous layered detonations bounded by an inert gas
Gaseous detonations propagating through a layer of reactants that is bounded by an inert gas were simulated by solving the two-dimensional reactive Euler equations. A single-step chemical reaction model was used with thermochemical properties that are representative of a highly reactive fuel–oxidize...
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Veröffentlicht in: | Combustion and flame 2017-05, Vol.179, p.185-198 |
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description | Gaseous detonations propagating through a layer of reactants that is bounded by an inert gas were simulated by solving the two-dimensional reactive Euler equations. A single-step chemical reaction model was used with thermochemical properties that are representative of a highly reactive fuel–oxidizer mixture, such as stoichiometric ethylene and oxygen. A series of cases with varying acoustic impedance ratios between the inert and reactant gases, Z, were studied to explore the influence of acoustic impedance mismatch on the propagation of a detonation through the reactant layer. The detonation failed when Z ∼ 1 due to a loss of triple points at the interface. The detonation propagated stably when Z is high and the impedance of the inert gas is much higher than the reactants. Reflected shocks are produced from the interaction of the Mach stem of a detonation cell with the interface between the reactant and inert gases. These reflected shocks, in turn, detach and generate new triple points that are necessary to propagate the detonation. The detonation was also stable when the acoustic impedance of the inert gas is much lower than the reactants. A gas dynamic structure forms that involves a detached shock in the inert gas and a series of oblique shocks and slip lines in the reactants. A small local explosion is triggered when the Mach stem of a detonation cell interacts with the compressed reactants behind one of these oblique shocks. The resulting retonation wave produces a new Mach stem and a new triple point that leads to a stable detonation. These results suggest that the acoustic impedance and shock structure in the inert gas can have a significant influence on the stable propagation of a layered gaseous detonation. |
doi_str_mv | 10.1016/j.combustflame.2017.02.001 |
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A single-step chemical reaction model was used with thermochemical properties that are representative of a highly reactive fuel–oxidizer mixture, such as stoichiometric ethylene and oxygen. A series of cases with varying acoustic impedance ratios between the inert and reactant gases, Z, were studied to explore the influence of acoustic impedance mismatch on the propagation of a detonation through the reactant layer. The detonation failed when Z ∼ 1 due to a loss of triple points at the interface. The detonation propagated stably when Z is high and the impedance of the inert gas is much higher than the reactants. Reflected shocks are produced from the interaction of the Mach stem of a detonation cell with the interface between the reactant and inert gases. These reflected shocks, in turn, detach and generate new triple points that are necessary to propagate the detonation. The detonation was also stable when the acoustic impedance of the inert gas is much lower than the reactants. A gas dynamic structure forms that involves a detached shock in the inert gas and a series of oblique shocks and slip lines in the reactants. A small local explosion is triggered when the Mach stem of a detonation cell interacts with the compressed reactants behind one of these oblique shocks. The resulting retonation wave produces a new Mach stem and a new triple point that leads to a stable detonation. These results suggest that the acoustic impedance and shock structure in the inert gas can have a significant influence on the stable propagation of a layered gaseous detonation.</description><identifier>ISSN: 0010-2180</identifier><identifier>EISSN: 1556-2921</identifier><identifier>DOI: 10.1016/j.combustflame.2017.02.001</identifier><language>eng</language><publisher>New York: Elsevier Inc</publisher><subject>Acoustic impedance ; Acoustic propagation ; Acoustics ; Computer simulation ; Detaching ; Detonation ; Diffusion ; Ethylene ; Euler-Lagrange equation ; Gases ; Impedance ; Layer ; Numerical analysis ; Numerical simulation ; Rare gases ; Shock wave ; Studies ; Thermochemical properties ; Two dimensional models ; Viscosity</subject><ispartof>Combustion and flame, 2017-05, Vol.179, p.185-198</ispartof><rights>2017 The Combustion Institute</rights><rights>Copyright Elsevier BV May 2017</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c470t-5944f092d39c9642eb3906ec17a7e70b080d425b41d019795c04baaa87eeb873</citedby><cites>FETCH-LOGICAL-c470t-5944f092d39c9642eb3906ec17a7e70b080d425b41d019795c04baaa87eeb873</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0010218017300299$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>Houim, Ryan W.</creatorcontrib><creatorcontrib>Fievisohn, Robert T.</creatorcontrib><title>The influence of acoustic impedance on gaseous layered detonations bounded by an inert gas</title><title>Combustion and flame</title><description>Gaseous detonations propagating through a layer of reactants that is bounded by an inert gas were simulated by solving the two-dimensional reactive Euler equations. A single-step chemical reaction model was used with thermochemical properties that are representative of a highly reactive fuel–oxidizer mixture, such as stoichiometric ethylene and oxygen. A series of cases with varying acoustic impedance ratios between the inert and reactant gases, Z, were studied to explore the influence of acoustic impedance mismatch on the propagation of a detonation through the reactant layer. The detonation failed when Z ∼ 1 due to a loss of triple points at the interface. The detonation propagated stably when Z is high and the impedance of the inert gas is much higher than the reactants. Reflected shocks are produced from the interaction of the Mach stem of a detonation cell with the interface between the reactant and inert gases. These reflected shocks, in turn, detach and generate new triple points that are necessary to propagate the detonation. The detonation was also stable when the acoustic impedance of the inert gas is much lower than the reactants. A gas dynamic structure forms that involves a detached shock in the inert gas and a series of oblique shocks and slip lines in the reactants. A small local explosion is triggered when the Mach stem of a detonation cell interacts with the compressed reactants behind one of these oblique shocks. The resulting retonation wave produces a new Mach stem and a new triple point that leads to a stable detonation. These results suggest that the acoustic impedance and shock structure in the inert gas can have a significant influence on the stable propagation of a layered gaseous detonation.</description><subject>Acoustic impedance</subject><subject>Acoustic propagation</subject><subject>Acoustics</subject><subject>Computer simulation</subject><subject>Detaching</subject><subject>Detonation</subject><subject>Diffusion</subject><subject>Ethylene</subject><subject>Euler-Lagrange equation</subject><subject>Gases</subject><subject>Impedance</subject><subject>Layer</subject><subject>Numerical analysis</subject><subject>Numerical simulation</subject><subject>Rare gases</subject><subject>Shock wave</subject><subject>Studies</subject><subject>Thermochemical properties</subject><subject>Two dimensional models</subject><subject>Viscosity</subject><issn>0010-2180</issn><issn>1556-2921</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNqNkE1LxDAQhoMouK7-h6Dn1kn6kcab-A0LXvbkJaTJVLO0zZq0wv57s64Hj54GHt55h3kIuWSQM2D19SY3fmjnOHW9HjDnwEQOPAdgR2TBqqrOuOTsmCwSgYyzBk7JWYwbABBlUSzI2_oDqRu7fsbRIPUd1canPmeoG7Zo9Q8d6buOmDjt9Q4DWmpx8qOenB8jbf082sTaHdVjKsMw7fPn5KTTfcSL37kk68eH9d1ztnp9erm7XWWmFDBllSzLDiS3hTSyLjm2hYQaDRNaoIAWGrAlr9qSWWBSyMpA2WqtG4HYNqJYkqtD7Tb4zxnjpDZ-DmO6qJjkFauBQ5NSN4eUCT7GgJ3aBjfosFMM1F6l2qi_KtVepQKukri0fH9YxvTGl8OgonF7X9YFNJOy3v2n5hsLaYP0</recordid><startdate>20170501</startdate><enddate>20170501</enddate><creator>Houim, Ryan W.</creator><creator>Fievisohn, Robert T.</creator><general>Elsevier Inc</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20170501</creationdate><title>The influence of acoustic impedance on gaseous layered detonations bounded by an inert gas</title><author>Houim, Ryan W. ; Fievisohn, Robert T.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c470t-5944f092d39c9642eb3906ec17a7e70b080d425b41d019795c04baaa87eeb873</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Acoustic impedance</topic><topic>Acoustic propagation</topic><topic>Acoustics</topic><topic>Computer simulation</topic><topic>Detaching</topic><topic>Detonation</topic><topic>Diffusion</topic><topic>Ethylene</topic><topic>Euler-Lagrange equation</topic><topic>Gases</topic><topic>Impedance</topic><topic>Layer</topic><topic>Numerical analysis</topic><topic>Numerical simulation</topic><topic>Rare gases</topic><topic>Shock wave</topic><topic>Studies</topic><topic>Thermochemical properties</topic><topic>Two dimensional models</topic><topic>Viscosity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Houim, Ryan W.</creatorcontrib><creatorcontrib>Fievisohn, Robert T.</creatorcontrib><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>Combustion and flame</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Houim, Ryan W.</au><au>Fievisohn, Robert T.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The influence of acoustic impedance on gaseous layered detonations bounded by an inert gas</atitle><jtitle>Combustion and flame</jtitle><date>2017-05-01</date><risdate>2017</risdate><volume>179</volume><spage>185</spage><epage>198</epage><pages>185-198</pages><issn>0010-2180</issn><eissn>1556-2921</eissn><abstract>Gaseous detonations propagating through a layer of reactants that is bounded by an inert gas were simulated by solving the two-dimensional reactive Euler equations. A single-step chemical reaction model was used with thermochemical properties that are representative of a highly reactive fuel–oxidizer mixture, such as stoichiometric ethylene and oxygen. A series of cases with varying acoustic impedance ratios between the inert and reactant gases, Z, were studied to explore the influence of acoustic impedance mismatch on the propagation of a detonation through the reactant layer. The detonation failed when Z ∼ 1 due to a loss of triple points at the interface. The detonation propagated stably when Z is high and the impedance of the inert gas is much higher than the reactants. Reflected shocks are produced from the interaction of the Mach stem of a detonation cell with the interface between the reactant and inert gases. These reflected shocks, in turn, detach and generate new triple points that are necessary to propagate the detonation. The detonation was also stable when the acoustic impedance of the inert gas is much lower than the reactants. A gas dynamic structure forms that involves a detached shock in the inert gas and a series of oblique shocks and slip lines in the reactants. A small local explosion is triggered when the Mach stem of a detonation cell interacts with the compressed reactants behind one of these oblique shocks. The resulting retonation wave produces a new Mach stem and a new triple point that leads to a stable detonation. These results suggest that the acoustic impedance and shock structure in the inert gas can have a significant influence on the stable propagation of a layered gaseous detonation.</abstract><cop>New York</cop><pub>Elsevier Inc</pub><doi>10.1016/j.combustflame.2017.02.001</doi><tpages>14</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Acoustic impedance Acoustic propagation Acoustics Computer simulation Detaching Detonation Diffusion Ethylene Euler-Lagrange equation Gases Impedance Layer Numerical analysis Numerical simulation Rare gases Shock wave Studies Thermochemical properties Two dimensional models Viscosity |
title | The influence of acoustic impedance on gaseous layered detonations bounded by an inert gas |
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