Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube
Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas an...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Wang, C. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2006 |
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| Schlagwörter: |
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| Anmerkung: |
© Springer-Verlag 2006 |
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| Übergeordnetes Werk: |
Enthalten in: Shock waves - Springer-Verlag, 1991, 15(2006), 2 vom: 06. Mai, Seite 129-135 |
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| Übergeordnetes Werk: |
volume:15 ; year:2006 ; number:2 ; day:06 ; month:05 ; pages:129-135 |
| Links: |
|---|
| DOI / URN: |
10.1007/s00193-006-0014-5 |
|---|
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OLC2057893855 |
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| 520 | |a Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. | ||
| 650 | 4 | |a Ignition | |
| 650 | 4 | |a Hydrocarbon fuel | |
| 650 | 4 | |a Shock focusing | |
| 650 | 4 | |a Separation mode of shock tube | |
| 700 | 1 | |a Han, Z. Y. |4 aut | |
| 700 | 1 | |a Situ, M. |4 aut | |
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10.1007/s00193-006-0014-5 doi (DE-627)OLC2057893855 (DE-He213)s00193-006-0014-5-p DE-627 ger DE-627 rakwb eng 530 VZ Wang, C. verfasserin aut Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube 2006 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2006 Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. Ignition Hydrocarbon fuel Shock focusing Separation mode of shock tube Han, Z. Y. aut Situ, M. aut Enthalten in Shock waves Springer-Verlag, 1991 15(2006), 2 vom: 06. Mai, Seite 129-135 (DE-627)130966657 (DE-600)1068310-0 (DE-576)025185977 0938-1287 nnns volume:15 year:2006 number:2 day:06 month:05 pages:129-135 https://doi.org/10.1007/s00193-006-0014-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_267 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_4277 GBV_ILN_4309 GBV_ILN_4700 AR 15 2006 2 06 05 129-135 |
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10.1007/s00193-006-0014-5 doi (DE-627)OLC2057893855 (DE-He213)s00193-006-0014-5-p DE-627 ger DE-627 rakwb eng 530 VZ Wang, C. verfasserin aut Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube 2006 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2006 Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. Ignition Hydrocarbon fuel Shock focusing Separation mode of shock tube Han, Z. Y. aut Situ, M. aut Enthalten in Shock waves Springer-Verlag, 1991 15(2006), 2 vom: 06. Mai, Seite 129-135 (DE-627)130966657 (DE-600)1068310-0 (DE-576)025185977 0938-1287 nnns volume:15 year:2006 number:2 day:06 month:05 pages:129-135 https://doi.org/10.1007/s00193-006-0014-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_267 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_4277 GBV_ILN_4309 GBV_ILN_4700 AR 15 2006 2 06 05 129-135 |
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10.1007/s00193-006-0014-5 doi (DE-627)OLC2057893855 (DE-He213)s00193-006-0014-5-p DE-627 ger DE-627 rakwb eng 530 VZ Wang, C. verfasserin aut Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube 2006 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2006 Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. Ignition Hydrocarbon fuel Shock focusing Separation mode of shock tube Han, Z. Y. aut Situ, M. aut Enthalten in Shock waves Springer-Verlag, 1991 15(2006), 2 vom: 06. Mai, Seite 129-135 (DE-627)130966657 (DE-600)1068310-0 (DE-576)025185977 0938-1287 nnns volume:15 year:2006 number:2 day:06 month:05 pages:129-135 https://doi.org/10.1007/s00193-006-0014-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_267 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_4277 GBV_ILN_4309 GBV_ILN_4700 AR 15 2006 2 06 05 129-135 |
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10.1007/s00193-006-0014-5 doi (DE-627)OLC2057893855 (DE-He213)s00193-006-0014-5-p DE-627 ger DE-627 rakwb eng 530 VZ Wang, C. verfasserin aut Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube 2006 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2006 Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. Ignition Hydrocarbon fuel Shock focusing Separation mode of shock tube Han, Z. Y. aut Situ, M. aut Enthalten in Shock waves Springer-Verlag, 1991 15(2006), 2 vom: 06. Mai, Seite 129-135 (DE-627)130966657 (DE-600)1068310-0 (DE-576)025185977 0938-1287 nnns volume:15 year:2006 number:2 day:06 month:05 pages:129-135 https://doi.org/10.1007/s00193-006-0014-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_267 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_4277 GBV_ILN_4309 GBV_ILN_4700 AR 15 2006 2 06 05 129-135 |
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10.1007/s00193-006-0014-5 doi (DE-627)OLC2057893855 (DE-He213)s00193-006-0014-5-p DE-627 ger DE-627 rakwb eng 530 VZ Wang, C. verfasserin aut Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube 2006 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer-Verlag 2006 Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. Ignition Hydrocarbon fuel Shock focusing Separation mode of shock tube Han, Z. Y. aut Situ, M. aut Enthalten in Shock waves Springer-Verlag, 1991 15(2006), 2 vom: 06. Mai, Seite 129-135 (DE-627)130966657 (DE-600)1068310-0 (DE-576)025185977 0938-1287 nnns volume:15 year:2006 number:2 day:06 month:05 pages:129-135 https://doi.org/10.1007/s00193-006-0014-5 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_40 GBV_ILN_70 GBV_ILN_267 GBV_ILN_2016 GBV_ILN_2018 GBV_ILN_4277 GBV_ILN_4309 GBV_ILN_4700 AR 15 2006 2 06 05 129-135 |
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Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube |
| abstract |
Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. © Springer-Verlag 2006 |
| abstractGer |
Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. © Springer-Verlag 2006 |
| abstract_unstemmed |
Abstract The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “line-flame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90m/s and the delay time of ignition is estimated in the range of 0.12–0.29ms. © Springer-Verlag 2006 |
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| container_issue |
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| title_short |
Investigation of high-speed combustible gas ignited by a hot gas jetproduced in the shock tube |
| url |
https://doi.org/10.1007/s00193-006-0014-5 |
| remote_bool |
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| author2 |
Han, Z. Y. Situ, M. |
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Han, Z. Y. Situ, M. |
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| doi_str |
10.1007/s00193-006-0014-5 |
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2024-07-03T16:45:59.164Z |
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