{"title":"不同湍流模型对超临界压力下横流受限射流模拟的评价","authors":"S. Janani, Komal Gada, H. Rahai, F. Davoudzadeh","doi":"10.1115/IMECE2018-87894","DOIUrl":null,"url":null,"abstract":"Numerical investigations of using two different turbulence models of K-ε and K-ω on mixing characteristics of two confined jets in a crossflow at supercritical pressure have been performed. The confined jets were at 180 degrees from each other injecting into a round tube. The jet to crossflow mass flows ratio, r, was 2.96. Reynolds Averaged Navier Stokes (RANS) equations were solved using Siemens PLM CCM+ software. Results indicate higher mixing rate with K-ω turbulence model. Higher vorticity and lower turbulent kinetic energy are observed with k-ω turbulence model. Increased mixing indicate reduced velocity and pressure gradients and cooler fluid toward the tube wall.","PeriodicalId":229616,"journal":{"name":"Volume 7: Fluids Engineering","volume":"146 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-11-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Assessment of Different Turbulence Models on Simulations of Confined Jets in a Crossflow at Supercritical Pressure\",\"authors\":\"S. Janani, Komal Gada, H. Rahai, F. Davoudzadeh\",\"doi\":\"10.1115/IMECE2018-87894\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Numerical investigations of using two different turbulence models of K-ε and K-ω on mixing characteristics of two confined jets in a crossflow at supercritical pressure have been performed. The confined jets were at 180 degrees from each other injecting into a round tube. The jet to crossflow mass flows ratio, r, was 2.96. Reynolds Averaged Navier Stokes (RANS) equations were solved using Siemens PLM CCM+ software. Results indicate higher mixing rate with K-ω turbulence model. Higher vorticity and lower turbulent kinetic energy are observed with k-ω turbulence model. Increased mixing indicate reduced velocity and pressure gradients and cooler fluid toward the tube wall.\",\"PeriodicalId\":229616,\"journal\":{\"name\":\"Volume 7: Fluids Engineering\",\"volume\":\"146 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-11-09\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Volume 7: Fluids Engineering\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1115/IMECE2018-87894\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Volume 7: Fluids Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/IMECE2018-87894","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
摘要
采用K-ε和K-ω两种不同的湍流模型,对超临界压力下横流中两束受限射流的混合特性进行了数值研究。封闭的射流彼此成180度,注入一个圆形管中。射流与横流的质量流量比r为2.96。采用Siemens PLM CCM+软件求解Reynolds average Navier Stokes (RANS)方程。结果表明,K-ω湍流模型具有较高的混合速率。在k-ω湍流模型下,可以观察到较高的涡度和较低的湍流动能。增加的混合表明速度和压力梯度降低,流体流向管壁变冷。
Assessment of Different Turbulence Models on Simulations of Confined Jets in a Crossflow at Supercritical Pressure
Numerical investigations of using two different turbulence models of K-ε and K-ω on mixing characteristics of two confined jets in a crossflow at supercritical pressure have been performed. The confined jets were at 180 degrees from each other injecting into a round tube. The jet to crossflow mass flows ratio, r, was 2.96. Reynolds Averaged Navier Stokes (RANS) equations were solved using Siemens PLM CCM+ software. Results indicate higher mixing rate with K-ω turbulence model. Higher vorticity and lower turbulent kinetic energy are observed with k-ω turbulence model. Increased mixing indicate reduced velocity and pressure gradients and cooler fluid toward the tube wall.