Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers
Combustion of ethylene and kerosene in flows with Mach numbers M 2 is numerically studied. Flow throttling with the use of a side jet of compressed air is provided for igniting the fuel injected through an axial injector and for supporting its combustion. The Reynolds-averaged Navier–Stokes equati...
Gespeichert in:
| Veröffentlicht in: | Combustion, explosion, and shock waves explosion, and shock waves, 2022-08, Vol.58 (4), p.450-456 |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 456 |
|---|---|
| container_issue | 4 |
| container_start_page | 450 |
| container_title | Combustion, explosion, and shock waves |
| container_volume | 58 |
| creator | Zamuraev, V. P. Kalinina, A. P. |
| description | Combustion of ethylene and kerosene in flows with Mach numbers M
2 is numerically studied. Flow throttling with the use of a side jet of compressed air is provided for igniting the fuel injected through an axial injector and for supporting its combustion. The Reynolds-averaged Navier–Stokes equations closed with the
–
turbulence model are solved. Fuel combustion is modeled by one reaction. The possibility of formation of a transonic flow is considered. The gas-dynamic structure of the flow in the channel in the case of kerosene combustion is investigated for the Mach number M = 1.7 and stagnation temperatures of 1400 and 1500 K. The computations are performed for various values of the limiter of turbulent kinetic energy generation. |
| doi_str_mv | 10.1134/S0010508222040074 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2715808867</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2715808867</sourcerecordid><originalsourceid>FETCH-LOGICAL-c246t-fd05b9b07ba9b6d82f5dce73c87d9e3b186ce8473fbf921dbe0713bc5be7906d3</originalsourceid><addsrcrecordid>eNp1UE1LwzAYDqLgnP4AbwHP1TdJ06RHGZsTqx6m55KkqevYkpm0yP69KRM8iKeHl-eL90HomsAtISy_WwEQ4CAppZADiPwETQgXLJMs56doMtLZyJ-jixg3AEBpXkxQNfM7PcS-8w77Fs_79WFrncXKNfjJBh_Ho3NY4dWwtyF61xm82PovrHpcJXhWZo1fhp1O5CU6a9U22qsfnKL3xfxttsyq14fH2X2VmdTZZ20DXJcahFalLhpJW94YK5iRoikt00QWxspcsFa3JSWNtiAI04ZrK0ooGjZFN8fcffCfg419vfFDcKmypoJwCVIWIqnIUWXSGzHYtt6HbqfCoSZQj6PVf0ZLHnr0xKR1Hzb8Jv9v-gb_LW1D</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2715808867</pqid></control><display><type>article</type><title>Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers</title><source>Springer Nature - Complete Springer Journals</source><creator>Zamuraev, V. P. ; Kalinina, A. P.</creator><creatorcontrib>Zamuraev, V. P. ; Kalinina, A. P.</creatorcontrib><description>Combustion of ethylene and kerosene in flows with Mach numbers M
2 is numerically studied. Flow throttling with the use of a side jet of compressed air is provided for igniting the fuel injected through an axial injector and for supporting its combustion. The Reynolds-averaged Navier–Stokes equations closed with the
–
turbulence model are solved. Fuel combustion is modeled by one reaction. The possibility of formation of a transonic flow is considered. The gas-dynamic structure of the flow in the channel in the case of kerosene combustion is investigated for the Mach number M = 1.7 and stagnation temperatures of 1400 and 1500 K. The computations are performed for various values of the limiter of turbulent kinetic energy generation.</description><identifier>ISSN: 0010-5082</identifier><identifier>EISSN: 1573-8345</identifier><identifier>DOI: 10.1134/S0010508222040074</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Classical and Continuum Physics ; Classical Mechanics ; Compressed air ; Control ; Dynamical Systems ; Engineering ; Ethylene ; Fuel combustion ; Kerosene ; Kinetic energy ; Mach number ; Physical Chemistry ; Physics ; Physics and Astronomy ; Reynolds averaged Navier-Stokes method ; Supersonic flow ; Throttling ; Transonic flow ; Turbulence models ; Turbulent flow ; Vibration</subject><ispartof>Combustion, explosion, and shock waves, 2022-08, Vol.58 (4), p.450-456</ispartof><rights>Pleiades Publishing, Ltd. 2022</rights><rights>Pleiades Publishing, Ltd. 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c246t-fd05b9b07ba9b6d82f5dce73c87d9e3b186ce8473fbf921dbe0713bc5be7906d3</citedby><cites>FETCH-LOGICAL-c246t-fd05b9b07ba9b6d82f5dce73c87d9e3b186ce8473fbf921dbe0713bc5be7906d3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1134/S0010508222040074$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1134/S0010508222040074$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Zamuraev, V. P.</creatorcontrib><creatorcontrib>Kalinina, A. P.</creatorcontrib><title>Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers</title><title>Combustion, explosion, and shock waves</title><addtitle>Combust Explos Shock Waves</addtitle><description>Combustion of ethylene and kerosene in flows with Mach numbers M
2 is numerically studied. Flow throttling with the use of a side jet of compressed air is provided for igniting the fuel injected through an axial injector and for supporting its combustion. The Reynolds-averaged Navier–Stokes equations closed with the
–
turbulence model are solved. Fuel combustion is modeled by one reaction. The possibility of formation of a transonic flow is considered. The gas-dynamic structure of the flow in the channel in the case of kerosene combustion is investigated for the Mach number M = 1.7 and stagnation temperatures of 1400 and 1500 K. The computations are performed for various values of the limiter of turbulent kinetic energy generation.</description><subject>Classical and Continuum Physics</subject><subject>Classical Mechanics</subject><subject>Compressed air</subject><subject>Control</subject><subject>Dynamical Systems</subject><subject>Engineering</subject><subject>Ethylene</subject><subject>Fuel combustion</subject><subject>Kerosene</subject><subject>Kinetic energy</subject><subject>Mach number</subject><subject>Physical Chemistry</subject><subject>Physics</subject><subject>Physics and Astronomy</subject><subject>Reynolds averaged Navier-Stokes method</subject><subject>Supersonic flow</subject><subject>Throttling</subject><subject>Transonic flow</subject><subject>Turbulence models</subject><subject>Turbulent flow</subject><subject>Vibration</subject><issn>0010-5082</issn><issn>1573-8345</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1UE1LwzAYDqLgnP4AbwHP1TdJ06RHGZsTqx6m55KkqevYkpm0yP69KRM8iKeHl-eL90HomsAtISy_WwEQ4CAppZADiPwETQgXLJMs56doMtLZyJ-jixg3AEBpXkxQNfM7PcS-8w77Fs_79WFrncXKNfjJBh_Ho3NY4dWwtyF61xm82PovrHpcJXhWZo1fhp1O5CU6a9U22qsfnKL3xfxttsyq14fH2X2VmdTZZ20DXJcahFalLhpJW94YK5iRoikt00QWxspcsFa3JSWNtiAI04ZrK0ooGjZFN8fcffCfg419vfFDcKmypoJwCVIWIqnIUWXSGzHYtt6HbqfCoSZQj6PVf0ZLHnr0xKR1Hzb8Jv9v-gb_LW1D</recordid><startdate>20220801</startdate><enddate>20220801</enddate><creator>Zamuraev, V. P.</creator><creator>Kalinina, A. P.</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20220801</creationdate><title>Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers</title><author>Zamuraev, V. P. ; Kalinina, A. P.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c246t-fd05b9b07ba9b6d82f5dce73c87d9e3b186ce8473fbf921dbe0713bc5be7906d3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Classical and Continuum Physics</topic><topic>Classical Mechanics</topic><topic>Compressed air</topic><topic>Control</topic><topic>Dynamical Systems</topic><topic>Engineering</topic><topic>Ethylene</topic><topic>Fuel combustion</topic><topic>Kerosene</topic><topic>Kinetic energy</topic><topic>Mach number</topic><topic>Physical Chemistry</topic><topic>Physics</topic><topic>Physics and Astronomy</topic><topic>Reynolds averaged Navier-Stokes method</topic><topic>Supersonic flow</topic><topic>Throttling</topic><topic>Transonic flow</topic><topic>Turbulence models</topic><topic>Turbulent flow</topic><topic>Vibration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zamuraev, V. P.</creatorcontrib><creatorcontrib>Kalinina, A. P.</creatorcontrib><collection>CrossRef</collection><jtitle>Combustion, explosion, and shock waves</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zamuraev, V. P.</au><au>Kalinina, A. P.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers</atitle><jtitle>Combustion, explosion, and shock waves</jtitle><stitle>Combust Explos Shock Waves</stitle><date>2022-08-01</date><risdate>2022</risdate><volume>58</volume><issue>4</issue><spage>450</spage><epage>456</epage><pages>450-456</pages><issn>0010-5082</issn><eissn>1573-8345</eissn><abstract>Combustion of ethylene and kerosene in flows with Mach numbers M
2 is numerically studied. Flow throttling with the use of a side jet of compressed air is provided for igniting the fuel injected through an axial injector and for supporting its combustion. The Reynolds-averaged Navier–Stokes equations closed with the
–
turbulence model are solved. Fuel combustion is modeled by one reaction. The possibility of formation of a transonic flow is considered. The gas-dynamic structure of the flow in the channel in the case of kerosene combustion is investigated for the Mach number M = 1.7 and stagnation temperatures of 1400 and 1500 K. The computations are performed for various values of the limiter of turbulent kinetic energy generation.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.1134/S0010508222040074</doi><tpages>7</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0010-5082 |
| ispartof | Combustion, explosion, and shock waves, 2022-08, Vol.58 (4), p.450-456 |
| issn | 0010-5082 1573-8345 |
| language | eng |
| recordid | cdi_proquest_journals_2715808867 |
| source | Springer Nature - Complete Springer Journals |
| subjects | Classical and Continuum Physics Classical Mechanics Compressed air Control Dynamical Systems Engineering Ethylene Fuel combustion Kerosene Kinetic energy Mach number Physical Chemistry Physics Physics and Astronomy Reynolds averaged Navier-Stokes method Supersonic flow Throttling Transonic flow Turbulence models Turbulent flow Vibration |
| title | Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T13%3A36%3A43IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Combustion%20of%20Ethylene%20and%20Kerosene%20in%20a%20Supersonic%20Flow%20at%20Low%20Mach%20Numbers&rft.jtitle=Combustion,%20explosion,%20and%20shock%20waves&rft.au=Zamuraev,%20V.%20P.&rft.date=2022-08-01&rft.volume=58&rft.issue=4&rft.spage=450&rft.epage=456&rft.pages=450-456&rft.issn=0010-5082&rft.eissn=1573-8345&rft_id=info:doi/10.1134/S0010508222040074&rft_dat=%3Cproquest_cross%3E2715808867%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2715808867&rft_id=info:pmid/&rfr_iscdi=true |