PLIF investigation of turbulent mixing in a model GT-combustor
This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including corr...
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description | This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated. |
doi_str_mv | 10.1063/5.0051886 |
format | Conference Proceeding |
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G.</creator><contributor>Fomin, Vasily ; Shiplyuk, Alexander</contributor><creatorcontrib>Savitskii, A. G. ; Fomin, Vasily ; Shiplyuk, Alexander</creatorcontrib><description>This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0051886</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Acetone ; Combustion chambers ; Data processing ; Fuel injection ; Gas turbines ; Nonuniformity ; Planar laser induced fluorescence ; Signal processing ; Turbulent mixing</subject><ispartof>AIP conference proceedings, 2021, Vol.2351 (1)</ispartof><rights>Author(s)</rights><rights>2021 Author(s). Published by AIP Publishing.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://pubs.aip.org/acp/article-lookup/doi/10.1063/5.0051886$$EHTML$$P50$$Gscitation$$H</linktohtml><link.rule.ids>309,310,314,780,784,789,790,794,4512,23930,23931,25140,27924,27925,76384</link.rule.ids></links><search><contributor>Fomin, Vasily</contributor><contributor>Shiplyuk, Alexander</contributor><creatorcontrib>Savitskii, A. G.</creatorcontrib><title>PLIF investigation of turbulent mixing in a model GT-combustor</title><title>AIP conference proceedings</title><description>This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated.</description><subject>Acetone</subject><subject>Combustion chambers</subject><subject>Data processing</subject><subject>Fuel injection</subject><subject>Gas turbines</subject><subject>Nonuniformity</subject><subject>Planar laser induced fluorescence</subject><subject>Signal processing</subject><subject>Turbulent mixing</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2021</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNp90E1LwzAYB_AgCs7pwW8Q8CZ0Pkmal14EGW4OBnqY4C0kbTIy1qamrei3t7qBN08PD_x4Xv4IXROYERDsjs8AOFFKnKAJ4ZxkUhBxiiYARZ7RnL2do4uu2wHQQko1Qfcv69UCh-bDdX3Ymj7EBkeP-yHZYe-aHtfhMzTbUWCD61i5PV5usjLWduj6mC7RmTf7zl0d6xS9Lh4386ds_bxczR_WWUuBiUzSoih5brnxRuWu8mZs8kIxMOCkoF4wIqRVirKSVZVVRHhKGOMWGLEO2BTdHOa2Kb4P4616F4fUjCs15YzkUEghRnV7UF0Z-t9fdJtCbdKXJqB_8tFcH_P5D3_E9Ad1W3n2DYs3ZFA</recordid><startdate>20210524</startdate><enddate>20210524</enddate><creator>Savitskii, A. G.</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20210524</creationdate><title>PLIF investigation of turbulent mixing in a model GT-combustor</title><author>Savitskii, A. G.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p2036-7299c54b5afa84edfa54b49830a0e762f63167b8823c3ddb816f21335b031be03</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Acetone</topic><topic>Combustion chambers</topic><topic>Data processing</topic><topic>Fuel injection</topic><topic>Gas turbines</topic><topic>Nonuniformity</topic><topic>Planar laser induced fluorescence</topic><topic>Signal processing</topic><topic>Turbulent mixing</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Savitskii, A. G.</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Savitskii, A. G.</au><au>Fomin, Vasily</au><au>Shiplyuk, Alexander</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>PLIF investigation of turbulent mixing in a model GT-combustor</atitle><btitle>AIP conference proceedings</btitle><date>2021-05-24</date><risdate>2021</risdate><volume>2351</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0051886</doi><tpages>6</tpages><oa>free_for_read</oa></addata></record> |
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source | AIP Journals Complete |
subjects | Acetone Combustion chambers Data processing Fuel injection Gas turbines Nonuniformity Planar laser induced fluorescence Signal processing Turbulent mixing |
title | PLIF investigation of turbulent mixing in a model GT-combustor |
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