Shangqing Tao , Jun Fang , Yuhang Chen , Yahong Yang , Wei Chu , Jingwu Wang , Wenlong Wang , Longhua Hu
{"title":"球形多孔气体燃烧器中浮力诱导低拉伸率稳定层流扩散火焰的研究","authors":"Shangqing Tao , Jun Fang , Yuhang Chen , Yahong Yang , Wei Chu , Jingwu Wang , Wenlong Wang , Longhua Hu","doi":"10.1016/j.ijheatmasstransfer.2025.127907","DOIUrl":null,"url":null,"abstract":"<div><div>The steady combustion behavior and stability range of methane, ethylene, and propane in a low stretch spherical counterflow burner were investigated. Ethylene had the widest fuel mass flux (<span><math><msup><mover><mi>m</mi><mo>˙</mo></mover><mrow><mo>″</mo></mrow></msup></math></span>) range of steady blue flame. A decreased buoyant stretch rate (<em>a</em><sub>b</sub>) reduced this steady range. The critical <span><math><msup><mover><mi>m</mi><mo>˙</mo></mover><mrow><mo>″</mo></mrow></msup></math></span> at the extinction limit of the low stretch flames were lower than that of the normal gravity, and ethylene had the lowest critical <span><math><msup><mover><mi>m</mi><mo>˙</mo></mover><mrow><mo>″</mo></mrow></msup></math></span> at the lowest <em>a</em><sub>b</sub>, indicating a wider steady fuel mass flux range for ethylene and a greater fire risk for microgravity low stretch flames. The ratio of the flame horizontal length to the vertical length (<em>l</em><sub>f</sub>/<em>y</em><sub>f</sub>) was quantified by a dimensionless parameter: <span><math><mrow><mi>P</mi><msup><mrow><mi>e</mi></mrow><mrow><mo>−</mo><mfrac><mn>4</mn><mn>5</mn></mfrac></mrow></msup><msup><mrow><mo>(</mo><mfrac><mstyle><mi>Δ</mi></mstyle><mrow><mi>F</mi><mi>r</mi></mrow></mfrac><mo>)</mo></mrow><mrow><mo>−</mo><mfrac><mn>1</mn><mn>5</mn></mfrac></mrow></msup><msup><mrow><mo>(</mo><mrow><mi>S</mi><mrow><mo>+</mo><mn>1</mn></mrow></mrow><mo>)</mo></mrow><mrow><mo>−</mo><mfrac><mn>6</mn><mn>5</mn></mfrac></mrow></msup></mrow></math></span>, which considered the combined effects of burner properties (described by Péclet number <em>Pe</em>), gravity/buoyancy effect (described by expansion parameter <span><math><mstyle><mi>Δ</mi></mstyle></math></span> and Froude number <em>Fr</em>) and fuel combustion process (described by chemical reaction characteristic parameter <em>S</em>). The flame temperature <em>T</em><sub>f</sub> for the fuels increased with increasing <em>u</em><sub>F</sub> and <em>a</em><sub>b</sub>, whereas <em>T</em><sub>f</sub> increased slowly when <em>u</em><sub>F</sub> was greater than the sooting limit <em>u</em><sub>F</sub> due to incomplete combustion with appreciable heat loss. The low stretch flame temperatures of the three fuels rank as C<sub>2</sub>H<sub>4</sub>>C<sub>3</sub>H<sub>8</sub>>CH<sub>4</sub> because of their different heats of combustion and heat losses. Both the gas-phase and solid-phase heat losses fractions were significant at low stretch rates. Solid-phase heat loss was vital to methane, which largely influenced its periodic flame hole instability near the extinction limit. This flame instability also extended the flammable range of methane at low stretch rates. This study can give instructions for microgravity combustion because a flame is usually initiated at low stretch rates under microgravity.</div></div>","PeriodicalId":336,"journal":{"name":"International Journal of Heat and Mass Transfer","volume":"256 ","pages":"Article 127907"},"PeriodicalIF":5.8000,"publicationDate":"2025-10-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A study of steady laminar diffusion flames at buoyancy-induced low stretch rates in a spherical porous gas burner\",\"authors\":\"Shangqing Tao , Jun Fang , Yuhang Chen , Yahong Yang , Wei Chu , Jingwu Wang , Wenlong Wang , Longhua Hu\",\"doi\":\"10.1016/j.ijheatmasstransfer.2025.127907\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The steady combustion behavior and stability range of methane, ethylene, and propane in a low stretch spherical counterflow burner were investigated. Ethylene had the widest fuel mass flux (<span><math><msup><mover><mi>m</mi><mo>˙</mo></mover><mrow><mo>″</mo></mrow></msup></math></span>) range of steady blue flame. A decreased buoyant stretch rate (<em>a</em><sub>b</sub>) reduced this steady range. The critical <span><math><msup><mover><mi>m</mi><mo>˙</mo></mover><mrow><mo>″</mo></mrow></msup></math></span> at the extinction limit of the low stretch flames were lower than that of the normal gravity, and ethylene had the lowest critical <span><math><msup><mover><mi>m</mi><mo>˙</mo></mover><mrow><mo>″</mo></mrow></msup></math></span> at the lowest <em>a</em><sub>b</sub>, indicating a wider steady fuel mass flux range for ethylene and a greater fire risk for microgravity low stretch flames. The ratio of the flame horizontal length to the vertical length (<em>l</em><sub>f</sub>/<em>y</em><sub>f</sub>) was quantified by a dimensionless parameter: <span><math><mrow><mi>P</mi><msup><mrow><mi>e</mi></mrow><mrow><mo>−</mo><mfrac><mn>4</mn><mn>5</mn></mfrac></mrow></msup><msup><mrow><mo>(</mo><mfrac><mstyle><mi>Δ</mi></mstyle><mrow><mi>F</mi><mi>r</mi></mrow></mfrac><mo>)</mo></mrow><mrow><mo>−</mo><mfrac><mn>1</mn><mn>5</mn></mfrac></mrow></msup><msup><mrow><mo>(</mo><mrow><mi>S</mi><mrow><mo>+</mo><mn>1</mn></mrow></mrow><mo>)</mo></mrow><mrow><mo>−</mo><mfrac><mn>6</mn><mn>5</mn></mfrac></mrow></msup></mrow></math></span>, which considered the combined effects of burner properties (described by Péclet number <em>Pe</em>), gravity/buoyancy effect (described by expansion parameter <span><math><mstyle><mi>Δ</mi></mstyle></math></span> and Froude number <em>Fr</em>) and fuel combustion process (described by chemical reaction characteristic parameter <em>S</em>). The flame temperature <em>T</em><sub>f</sub> for the fuels increased with increasing <em>u</em><sub>F</sub> and <em>a</em><sub>b</sub>, whereas <em>T</em><sub>f</sub> increased slowly when <em>u</em><sub>F</sub> was greater than the sooting limit <em>u</em><sub>F</sub> due to incomplete combustion with appreciable heat loss. The low stretch flame temperatures of the three fuels rank as C<sub>2</sub>H<sub>4</sub>>C<sub>3</sub>H<sub>8</sub>>CH<sub>4</sub> because of their different heats of combustion and heat losses. Both the gas-phase and solid-phase heat losses fractions were significant at low stretch rates. Solid-phase heat loss was vital to methane, which largely influenced its periodic flame hole instability near the extinction limit. This flame instability also extended the flammable range of methane at low stretch rates. This study can give instructions for microgravity combustion because a flame is usually initiated at low stretch rates under microgravity.</div></div>\",\"PeriodicalId\":336,\"journal\":{\"name\":\"International Journal of Heat and Mass Transfer\",\"volume\":\"256 \",\"pages\":\"Article 127907\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-10-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Heat and Mass Transfer\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0017931025012426\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Heat and Mass Transfer","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0017931025012426","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
A study of steady laminar diffusion flames at buoyancy-induced low stretch rates in a spherical porous gas burner
The steady combustion behavior and stability range of methane, ethylene, and propane in a low stretch spherical counterflow burner were investigated. Ethylene had the widest fuel mass flux () range of steady blue flame. A decreased buoyant stretch rate (ab) reduced this steady range. The critical at the extinction limit of the low stretch flames were lower than that of the normal gravity, and ethylene had the lowest critical at the lowest ab, indicating a wider steady fuel mass flux range for ethylene and a greater fire risk for microgravity low stretch flames. The ratio of the flame horizontal length to the vertical length (lf/yf) was quantified by a dimensionless parameter: , which considered the combined effects of burner properties (described by Péclet number Pe), gravity/buoyancy effect (described by expansion parameter and Froude number Fr) and fuel combustion process (described by chemical reaction characteristic parameter S). The flame temperature Tf for the fuels increased with increasing uF and ab, whereas Tf increased slowly when uF was greater than the sooting limit uF due to incomplete combustion with appreciable heat loss. The low stretch flame temperatures of the three fuels rank as C2H4>C3H8>CH4 because of their different heats of combustion and heat losses. Both the gas-phase and solid-phase heat losses fractions were significant at low stretch rates. Solid-phase heat loss was vital to methane, which largely influenced its periodic flame hole instability near the extinction limit. This flame instability also extended the flammable range of methane at low stretch rates. This study can give instructions for microgravity combustion because a flame is usually initiated at low stretch rates under microgravity.
期刊介绍:
International Journal of Heat and Mass Transfer is the vehicle for the exchange of basic ideas in heat and mass transfer between research workers and engineers throughout the world. It focuses on both analytical and experimental research, with an emphasis on contributions which increase the basic understanding of transfer processes and their application to engineering problems.
Topics include:
-New methods of measuring and/or correlating transport-property data
-Energy engineering
-Environmental applications of heat and/or mass transfer