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Analytical investigation of non-adiabatic effects on the dynamics of sound reflection and transmission in a combustor
•By increasing cooling, the reflection is subsided, while the transmission is raised.•The variation of transmission by cooling is much larger than the reflection.•The response value is more altered by cooling when a subcritical nozzle is attached at the system outlet. Acoustics of a simplified, non-...
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Published in: | Applied thermal engineering 2016-04, Vol.98, p.553-567 |
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creator | Hosseinalipour, S.M. Fattahi, A. Karimi, N. |
description | •By increasing cooling, the reflection is subsided, while the transmission is raised.•The variation of transmission by cooling is much larger than the reflection.•The response value is more altered by cooling when a subcritical nozzle is attached at the system outlet.
Acoustics of a simplified, non-adiabatic combustor chamber, including a duct followed by a downstream exit nozzle, are considered. This system features heat transfer to the environment, and therefore involves mean axial temperature gradient along the duct and the nozzle. The effect of heat transfer on the dynamics of the acoustic reflection and transmission in the duct and nozzle is investigated analytically. These involve the development of analytical expressions for the response of non-adiabatic nozzles through compact acoustic modeling and also the effective length approach. Further, an existing work on the dynamics of heat transferring ducts is extended and combined with that of the nozzles. The acoustic responses of the combined non-adiabatic system are, subsequently, characterized by analyzing the net reflection and transmission of an incident acoustic wave. The results show that heat transfer can considerably modify the dynamic behavior of the acoustic reflections and transmissions. Due to the multiple reflections in the system, the phase response features significant irregularities. It is argued that the observed modifications in the chamber acoustics can noticeably affect the thermoacoustics of the system. |
doi_str_mv | 10.1016/j.applthermaleng.2015.12.116 |
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Acoustics of a simplified, non-adiabatic combustor chamber, including a duct followed by a downstream exit nozzle, are considered. This system features heat transfer to the environment, and therefore involves mean axial temperature gradient along the duct and the nozzle. The effect of heat transfer on the dynamics of the acoustic reflection and transmission in the duct and nozzle is investigated analytically. These involve the development of analytical expressions for the response of non-adiabatic nozzles through compact acoustic modeling and also the effective length approach. Further, an existing work on the dynamics of heat transferring ducts is extended and combined with that of the nozzles. The acoustic responses of the combined non-adiabatic system are, subsequently, characterized by analyzing the net reflection and transmission of an incident acoustic wave. The results show that heat transfer can considerably modify the dynamic behavior of the acoustic reflections and transmissions. Due to the multiple reflections in the system, the phase response features significant irregularities. It is argued that the observed modifications in the chamber acoustics can noticeably affect the thermoacoustics of the system.</description><identifier>ISSN: 1359-4311</identifier><identifier>DOI: 10.1016/j.applthermaleng.2015.12.116</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Acoustics ; Combustor and nozzle system ; Ducts ; Dynamical systems ; Dynamics ; Heat transfer ; Mathematical analysis ; Nozzles ; Reflection ; Sound reflection ; Sound transmission ; Thermoacoustic response</subject><ispartof>Applied thermal engineering, 2016-04, Vol.98, p.553-567</ispartof><rights>2015 Elsevier Ltd</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c417t-e7b41ffe7e46cbd06db18cfb7ff7beaf9fe3bca5298b6084ada628ac21500e7a3</citedby><cites>FETCH-LOGICAL-c417t-e7b41ffe7e46cbd06db18cfb7ff7beaf9fe3bca5298b6084ada628ac21500e7a3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Hosseinalipour, S.M.</creatorcontrib><creatorcontrib>Fattahi, A.</creatorcontrib><creatorcontrib>Karimi, N.</creatorcontrib><title>Analytical investigation of non-adiabatic effects on the dynamics of sound reflection and transmission in a combustor</title><title>Applied thermal engineering</title><description>•By increasing cooling, the reflection is subsided, while the transmission is raised.•The variation of transmission by cooling is much larger than the reflection.•The response value is more altered by cooling when a subcritical nozzle is attached at the system outlet.
Acoustics of a simplified, non-adiabatic combustor chamber, including a duct followed by a downstream exit nozzle, are considered. This system features heat transfer to the environment, and therefore involves mean axial temperature gradient along the duct and the nozzle. The effect of heat transfer on the dynamics of the acoustic reflection and transmission in the duct and nozzle is investigated analytically. These involve the development of analytical expressions for the response of non-adiabatic nozzles through compact acoustic modeling and also the effective length approach. Further, an existing work on the dynamics of heat transferring ducts is extended and combined with that of the nozzles. The acoustic responses of the combined non-adiabatic system are, subsequently, characterized by analyzing the net reflection and transmission of an incident acoustic wave. The results show that heat transfer can considerably modify the dynamic behavior of the acoustic reflections and transmissions. Due to the multiple reflections in the system, the phase response features significant irregularities. It is argued that the observed modifications in the chamber acoustics can noticeably affect the thermoacoustics of the system.</description><subject>Acoustics</subject><subject>Combustor and nozzle system</subject><subject>Ducts</subject><subject>Dynamical systems</subject><subject>Dynamics</subject><subject>Heat transfer</subject><subject>Mathematical analysis</subject><subject>Nozzles</subject><subject>Reflection</subject><subject>Sound reflection</subject><subject>Sound transmission</subject><subject>Thermoacoustic response</subject><issn>1359-4311</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNqNkDtPwzAUhTOARHn8hwwMLAm-eVdiqSoKSJVYYLauneviKrGL7VTqv8dRWdiYLB-fc6_PlyT3wHJg0DzuczwchvBFbsSBzC4vGNQ5FDlAc5EsoKyXWVUCXCXX3u8Zg6Jrq0UyrQwOp6AlDqk2R_JB7zBoa1KrUmNNhr1GERWZklIkg0_jW1yT9ieDo5Z-Nno7mT51pIbomMMYr8Gh8aP2fhZ01FJpRzH5YN1tcqlw8HT3e94kn5vnj_Vrtn1_eVuvtpmsoA0ZtaKCuLWlqpGiZ00voJNKtEq1glAtFZVCYl0sO9GwrsIem6JDWUDNGLVY3iQP57kHZ7-nWI7H_0gaBjRkJ8-hK-qqqRqAaH06W6Wz3scq_OD0iO7EgfGZMN_zv4T5TJhDwSPhGN-c4xTrHDU57qUmI6nXLjLhvdX_G_QDdeCT9g</recordid><startdate>20160405</startdate><enddate>20160405</enddate><creator>Hosseinalipour, S.M.</creator><creator>Fattahi, A.</creator><creator>Karimi, N.</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>KR7</scope></search><sort><creationdate>20160405</creationdate><title>Analytical investigation of non-adiabatic effects on the dynamics of sound reflection and transmission in a combustor</title><author>Hosseinalipour, S.M. ; Fattahi, A. ; Karimi, N.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c417t-e7b41ffe7e46cbd06db18cfb7ff7beaf9fe3bca5298b6084ada628ac21500e7a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Acoustics</topic><topic>Combustor and nozzle system</topic><topic>Ducts</topic><topic>Dynamical systems</topic><topic>Dynamics</topic><topic>Heat transfer</topic><topic>Mathematical analysis</topic><topic>Nozzles</topic><topic>Reflection</topic><topic>Sound reflection</topic><topic>Sound transmission</topic><topic>Thermoacoustic response</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hosseinalipour, S.M.</creatorcontrib><creatorcontrib>Fattahi, A.</creatorcontrib><creatorcontrib>Karimi, N.</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><jtitle>Applied thermal engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hosseinalipour, S.M.</au><au>Fattahi, A.</au><au>Karimi, N.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Analytical investigation of non-adiabatic effects on the dynamics of sound reflection and transmission in a combustor</atitle><jtitle>Applied thermal engineering</jtitle><date>2016-04-05</date><risdate>2016</risdate><volume>98</volume><spage>553</spage><epage>567</epage><pages>553-567</pages><issn>1359-4311</issn><abstract>•By increasing cooling, the reflection is subsided, while the transmission is raised.•The variation of transmission by cooling is much larger than the reflection.•The response value is more altered by cooling when a subcritical nozzle is attached at the system outlet.
Acoustics of a simplified, non-adiabatic combustor chamber, including a duct followed by a downstream exit nozzle, are considered. This system features heat transfer to the environment, and therefore involves mean axial temperature gradient along the duct and the nozzle. The effect of heat transfer on the dynamics of the acoustic reflection and transmission in the duct and nozzle is investigated analytically. These involve the development of analytical expressions for the response of non-adiabatic nozzles through compact acoustic modeling and also the effective length approach. Further, an existing work on the dynamics of heat transferring ducts is extended and combined with that of the nozzles. The acoustic responses of the combined non-adiabatic system are, subsequently, characterized by analyzing the net reflection and transmission of an incident acoustic wave. The results show that heat transfer can considerably modify the dynamic behavior of the acoustic reflections and transmissions. Due to the multiple reflections in the system, the phase response features significant irregularities. It is argued that the observed modifications in the chamber acoustics can noticeably affect the thermoacoustics of the system.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.applthermaleng.2015.12.116</doi><tpages>15</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Acoustics Combustor and nozzle system Ducts Dynamical systems Dynamics Heat transfer Mathematical analysis Nozzles Reflection Sound reflection Sound transmission Thermoacoustic response |
title | Analytical investigation of non-adiabatic effects on the dynamics of sound reflection and transmission in a combustor |
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