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Numerical and experimental verification of initial, transitional and turbulent regions of free turbulent round jet

机译:自由湍流圆形射流的初始,过渡和湍流区域的数值和实验验证

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Three-dimensional simulation of the whole domain (initial, transition and fully developed regions) of round jet is essential in order to predict and to study the flow behavior of multiple jets (e.g. confluent jets). According to authors knowledge, numerical prediction of round jet with RANS models that has been presented by other researchers, are only in two-dimensional (axisymmetric) and mostly for the fully developed region. The inlet boundary conditions, inlet velocity profile, turbulent kinetic energy and its dissipation rate at the diffuser exit has been governed from an earlier verified numerical simulation. In the present paper, results of three-dimensional modeling of isothermal, free, turbulent round jet with two two-equation (Low Re k - e and SST k - ω), a transition three-equation (k- kl- ω) and a transition four-equation (SST) eddy-viscosity turbulence models with resolved inlet profiles are compared and validated with hot-wire anemometry. This study shows that numerical simulation of round jet with SST k - ω gives good agreement with measured mean longitudinal velocities, while transition models could only predict the initial region of round jet.
机译:为了预测和研究多股射流(例如汇合射流)的流动行为,对圆形射流的整个域(初始,过渡和完全展开的区域)进行三维模拟是必不可少的。根据作者的知识,其他研究人员提出的使用RANS模型进行的圆形射流的数值预测仅在二维(轴对称)范围内,并且大部分用于完全发达的地区。入口边界条件,入口速度曲线,湍流动能及其在扩压器出口处的耗散率已通过较早验证的数值模拟进行了控制。在本文中,对具有两个两个方程式(低Re k-e和SST k-ω),一个过渡三方程式(k- kl-ω)和等温,自由,湍流的圆形射流进行三维建模的结果比较了具有解析的入口轮廓的过渡四方程(SST)涡流湍流模型,并通过热线风速仪进行了验证。这项研究表明,采用SST k-ω进行的圆形射流的数值模拟与测得的平均纵向速度具有良好的一致性,而过渡模型只能预测圆形射流的初始区域。

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