{"title":"欧拉-拉格朗日喷雾雾化模型中应力源系数的现场估算","authors":"C. R. L. Anumolu, Ambarish Dahale","doi":"10.4271/2024-01-5069","DOIUrl":null,"url":null,"abstract":"Liquid jet atomization is one of the key processes in many engineering\n applications, such as IC engines, gas turbines, and the like, to name a few.\n Simulating this process using a pure Eulerian or a pure Lagrangian framework has\n its own drawbacks. The Eulerian–Lagrangian spray atomization (ELSA) modeling\n seems like a viable alternative in such scenarios. ELSA simulations consist of\n solving an additional transport equation for the surface area density (Σ) of the\n issuing jet. In this study we have proposed a dynamic approach to compute the\n turbulent timescale constant (α1), which appears in\n the source of Σ-transport equation and is responsible for restoring the surface\n area back to its equilibrium. The dynamic approach involves an analytical\n computation of the turbulent timescale constant\n (α1), thereby eliminating the need for ad hoc\n adjustments to surface area values during computational fluid dynamics (CFD)\n simulations. Unlike previous research which suggests using constant values in\n the range (0, 1] for the α1-constant, we found that\n these values can be as high as 60,000 for the engine combustion network (ECN)\n spray-A nozzle conditions. The analytical closure procedure dampens the spurious\n overshoots seen in the sigma-Y field and maintains values close to the\n equilibrium conditions. The proposed approach is implemented in CONVERGE, a\n commercially available CFD code and validated by comparing against available\n experimental data.","PeriodicalId":510086,"journal":{"name":"SAE Technical Paper Series","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2024-07-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"In Situ Estimation of the Coefficient of Stress Source in the\\n Eulerian–Lagrangian Spray Atomization Model\",\"authors\":\"C. R. L. Anumolu, Ambarish Dahale\",\"doi\":\"10.4271/2024-01-5069\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Liquid jet atomization is one of the key processes in many engineering\\n applications, such as IC engines, gas turbines, and the like, to name a few.\\n Simulating this process using a pure Eulerian or a pure Lagrangian framework has\\n its own drawbacks. The Eulerian–Lagrangian spray atomization (ELSA) modeling\\n seems like a viable alternative in such scenarios. ELSA simulations consist of\\n solving an additional transport equation for the surface area density (Σ) of the\\n issuing jet. In this study we have proposed a dynamic approach to compute the\\n turbulent timescale constant (α1), which appears in\\n the source of Σ-transport equation and is responsible for restoring the surface\\n area back to its equilibrium. The dynamic approach involves an analytical\\n computation of the turbulent timescale constant\\n (α1), thereby eliminating the need for ad hoc\\n adjustments to surface area values during computational fluid dynamics (CFD)\\n simulations. Unlike previous research which suggests using constant values in\\n the range (0, 1] for the α1-constant, we found that\\n these values can be as high as 60,000 for the engine combustion network (ECN)\\n spray-A nozzle conditions. The analytical closure procedure dampens the spurious\\n overshoots seen in the sigma-Y field and maintains values close to the\\n equilibrium conditions. The proposed approach is implemented in CONVERGE, a\\n commercially available CFD code and validated by comparing against available\\n experimental data.\",\"PeriodicalId\":510086,\"journal\":{\"name\":\"SAE Technical Paper Series\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-07-03\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"SAE Technical Paper Series\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.4271/2024-01-5069\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"SAE Technical Paper Series","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4271/2024-01-5069","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
In Situ Estimation of the Coefficient of Stress Source in the
Eulerian–Lagrangian Spray Atomization Model
Liquid jet atomization is one of the key processes in many engineering
applications, such as IC engines, gas turbines, and the like, to name a few.
Simulating this process using a pure Eulerian or a pure Lagrangian framework has
its own drawbacks. The Eulerian–Lagrangian spray atomization (ELSA) modeling
seems like a viable alternative in such scenarios. ELSA simulations consist of
solving an additional transport equation for the surface area density (Σ) of the
issuing jet. In this study we have proposed a dynamic approach to compute the
turbulent timescale constant (α1), which appears in
the source of Σ-transport equation and is responsible for restoring the surface
area back to its equilibrium. The dynamic approach involves an analytical
computation of the turbulent timescale constant
(α1), thereby eliminating the need for ad hoc
adjustments to surface area values during computational fluid dynamics (CFD)
simulations. Unlike previous research which suggests using constant values in
the range (0, 1] for the α1-constant, we found that
these values can be as high as 60,000 for the engine combustion network (ECN)
spray-A nozzle conditions. The analytical closure procedure dampens the spurious
overshoots seen in the sigma-Y field and maintains values close to the
equilibrium conditions. The proposed approach is implemented in CONVERGE, a
commercially available CFD code and validated by comparing against available
experimental data.