{"title":"同轴双旋涡喷射器的近场混合","authors":"Sylvain Marragou, Thibault Frédéric Guiberti, Thierry Poinsot, Thierry Schuller","doi":"10.1007/s10494-024-00596-6","DOIUrl":null,"url":null,"abstract":"<div><p>Improving mixing between two coaxial swirled jets is a subject of interest for the development of next generations of fuel injectors. This is particularly crucial for hydrogen injectors, where the separate introduction of fuel and oxidizer is preferred to mitigate the risk of flashback. Raman scattering is used to measure the mean compositions and to examine how mixing between fuel and air streams evolves along the axial direction in the near-field of the injector outlet. The parameters kept constant include the swirl level <span>\\(S_e = 0.67\\)</span> in the annular channel, the injector dimensions, and the composition of the oxidizer stream, which is air. Experiments are carried out in cold flow conditions for different compositions of the central stream, including hydrogen and methane but also helium and argon. Three dimensionless mixing parameters are identified, the velocity ratio <span>\\(u_e/u_i\\)</span> between the external stream and internal stream, the density ratio <span>\\(\\rho _e/\\rho _i\\)</span> between the two fluids, and the inner swirl level <span>\\(S_i\\)</span> in the central channel. Adding swirl to the central jet significantly enhances mixing between the two streams very close to the injector outlet. Mixing also increases with higher velocity ratios <span>\\(u_e/u_i\\)</span>, independently of the inner swirl. Additionally, higher density ratios <span>\\(\\rho _e/\\rho _i\\)</span> enhance mixing between the two streams only in the case without swirl conferred to the central flow. A model is proposed for coaxial swirled jets, yielding a dimensionless mixing progress parameter that only depends on the velocity ratio <span>\\(u_e/u_i\\)</span> and geometrical features of the swirling flow that can be determined by examining the structure of the velocity field. Comparing the model with experiments, it is shown to perform effectively across the entire range of velocity ratios <span>\\(0.6 \\le u_e/u_i \\le 3.8\\)</span>, density ratios <span>\\(0.7 \\le \\rho _e/\\rho _i \\le 14.4\\)</span>, and inner swirl levels <span>\\(0.0 \\le S_i \\le 0.9\\)</span>. This law may be used to facilitate the design of coaxial swirled injectors.\n</p></div>","PeriodicalId":559,"journal":{"name":"Flow, Turbulence and Combustion","volume":"114 1","pages":"221 - 242"},"PeriodicalIF":2.0000,"publicationDate":"2024-11-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://link.springer.com/content/pdf/10.1007/s10494-024-00596-6.pdf","citationCount":"0","resultStr":"{\"title\":\"Near-Field Mixing in a Coaxial Dual Swirled Injector\",\"authors\":\"Sylvain Marragou, Thibault Frédéric Guiberti, Thierry Poinsot, Thierry Schuller\",\"doi\":\"10.1007/s10494-024-00596-6\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Improving mixing between two coaxial swirled jets is a subject of interest for the development of next generations of fuel injectors. This is particularly crucial for hydrogen injectors, where the separate introduction of fuel and oxidizer is preferred to mitigate the risk of flashback. Raman scattering is used to measure the mean compositions and to examine how mixing between fuel and air streams evolves along the axial direction in the near-field of the injector outlet. The parameters kept constant include the swirl level <span>\\\\(S_e = 0.67\\\\)</span> in the annular channel, the injector dimensions, and the composition of the oxidizer stream, which is air. Experiments are carried out in cold flow conditions for different compositions of the central stream, including hydrogen and methane but also helium and argon. Three dimensionless mixing parameters are identified, the velocity ratio <span>\\\\(u_e/u_i\\\\)</span> between the external stream and internal stream, the density ratio <span>\\\\(\\\\rho _e/\\\\rho _i\\\\)</span> between the two fluids, and the inner swirl level <span>\\\\(S_i\\\\)</span> in the central channel. Adding swirl to the central jet significantly enhances mixing between the two streams very close to the injector outlet. Mixing also increases with higher velocity ratios <span>\\\\(u_e/u_i\\\\)</span>, independently of the inner swirl. Additionally, higher density ratios <span>\\\\(\\\\rho _e/\\\\rho _i\\\\)</span> enhance mixing between the two streams only in the case without swirl conferred to the central flow. A model is proposed for coaxial swirled jets, yielding a dimensionless mixing progress parameter that only depends on the velocity ratio <span>\\\\(u_e/u_i\\\\)</span> and geometrical features of the swirling flow that can be determined by examining the structure of the velocity field. Comparing the model with experiments, it is shown to perform effectively across the entire range of velocity ratios <span>\\\\(0.6 \\\\le u_e/u_i \\\\le 3.8\\\\)</span>, density ratios <span>\\\\(0.7 \\\\le \\\\rho _e/\\\\rho _i \\\\le 14.4\\\\)</span>, and inner swirl levels <span>\\\\(0.0 \\\\le S_i \\\\le 0.9\\\\)</span>. This law may be used to facilitate the design of coaxial swirled injectors.\\n</p></div>\",\"PeriodicalId\":559,\"journal\":{\"name\":\"Flow, Turbulence and Combustion\",\"volume\":\"114 1\",\"pages\":\"221 - 242\"},\"PeriodicalIF\":2.0000,\"publicationDate\":\"2024-11-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://link.springer.com/content/pdf/10.1007/s10494-024-00596-6.pdf\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Flow, Turbulence and Combustion\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s10494-024-00596-6\",\"RegionNum\":3,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"MECHANICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Flow, Turbulence and Combustion","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s10494-024-00596-6","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MECHANICS","Score":null,"Total":0}
Near-Field Mixing in a Coaxial Dual Swirled Injector
Improving mixing between two coaxial swirled jets is a subject of interest for the development of next generations of fuel injectors. This is particularly crucial for hydrogen injectors, where the separate introduction of fuel and oxidizer is preferred to mitigate the risk of flashback. Raman scattering is used to measure the mean compositions and to examine how mixing between fuel and air streams evolves along the axial direction in the near-field of the injector outlet. The parameters kept constant include the swirl level \(S_e = 0.67\) in the annular channel, the injector dimensions, and the composition of the oxidizer stream, which is air. Experiments are carried out in cold flow conditions for different compositions of the central stream, including hydrogen and methane but also helium and argon. Three dimensionless mixing parameters are identified, the velocity ratio \(u_e/u_i\) between the external stream and internal stream, the density ratio \(\rho _e/\rho _i\) between the two fluids, and the inner swirl level \(S_i\) in the central channel. Adding swirl to the central jet significantly enhances mixing between the two streams very close to the injector outlet. Mixing also increases with higher velocity ratios \(u_e/u_i\), independently of the inner swirl. Additionally, higher density ratios \(\rho _e/\rho _i\) enhance mixing between the two streams only in the case without swirl conferred to the central flow. A model is proposed for coaxial swirled jets, yielding a dimensionless mixing progress parameter that only depends on the velocity ratio \(u_e/u_i\) and geometrical features of the swirling flow that can be determined by examining the structure of the velocity field. Comparing the model with experiments, it is shown to perform effectively across the entire range of velocity ratios \(0.6 \le u_e/u_i \le 3.8\), density ratios \(0.7 \le \rho _e/\rho _i \le 14.4\), and inner swirl levels \(0.0 \le S_i \le 0.9\). This law may be used to facilitate the design of coaxial swirled injectors.
期刊介绍:
Flow, Turbulence and Combustion provides a global forum for the publication of original and innovative research results that contribute to the solution of fundamental and applied problems encountered in single-phase, multi-phase and reacting flows, in both idealized and real systems. The scope of coverage encompasses topics in fluid dynamics, scalar transport, multi-physics interactions and flow control. From time to time the journal publishes Special or Theme Issues featuring invited articles.
Contributions may report research that falls within the broad spectrum of analytical, computational and experimental methods. This includes research conducted in academia, industry and a variety of environmental and geophysical sectors. Turbulence, transition and associated phenomena are expected to play a significant role in the majority of studies reported, although non-turbulent flows, typical of those in micro-devices, would be regarded as falling within the scope covered. The emphasis is on originality, timeliness, quality and thematic fit, as exemplified by the title of the journal and the qualifications described above. Relevance to real-world problems and industrial applications are regarded as strengths.