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ON THE ROLE OF THE DETERMINISTIC AND CIRCUMFERENTIAL STRESSES IN THROUGHFLOW CALCULATIONS

机译:确定性和周向应力在流量计算中的作用

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This paper presents a throughflow analysis tool developed in the context of the average-passage flow model elaborated by Adamczyk. The Adamczyk's flow model describes the 3-D time-averaged flow field within a blade row passage. The set of equations that governs this flow field is obtained by performing a Reynolds averaging, a time averaging and a passage-to-passage averaging on the Navier-Stokes equations. The throughflow level of approximation is obtained by performing an additional circumferential averaging on the 3-D average-passage flow.The resulting set of equations is similar to the 2-D axisym-metric Navier-Stokes equations but additional terms resulting from the averages show up : blade forces, blade blockage factor, Reynolds stresses, deterministic stresses, passage-to-passage stresses and circumferential stresses. This set of equations represents the ultimate throughflow model provided that all stresses and blade forces can be modeled. The relative importance of these additional terms is studied in the present contribution.The stresses and the blade forces are determined from 3-D steady and unsteady databases (a low speed compressor stage and a transonic turbine stage) and incorporated in a through-flow model based on the axisymmetric Navier-Stokes equations. A good agreement between the throughflow solution and the averaged 3-D results is obtained. These results are also compared to those obtained with a more "classical" throughflow approach based on a Navier-Stokes formulation for the endwall losses, correlations for profile losses and a simple radial mixing model assuming turbulent diffusion.
机译:本文介绍了在Adamczyk阐述的平均流量模型的背景下开发的通流分析工具。 Adamczyk的流动模型描述了叶片行通道内的3-D时间平均流场。通过对Navier-Stokes方程执行雷诺平均,时间平均和通道通过平均,可以得到控制此流场的一组方程式。通过对3-D平均通道流量执行附加的周向平均,可以得出近似的通流水平。 所得的方程组类似于二维轴对称的Navier-Stokes方程,但由平均值得出的其他项却出现了:叶片力,叶片堵塞因子,雷诺应力,确定性应力,通道间应力和周向应力压力。只要可以对所有应力和叶片力进行建模,这组方程式就代表了最终的通流模型。在本文稿中研究了这些附加术语的相对重要性。 应力和叶片力由3-D稳态和非稳态数据库(低速压缩机级和跨音速涡轮级)确定,并包含在基于轴对称Navier-Stokes方程的通流模型中。通流解决方案与平均3-D结果之间取得了良好的一致性。这些结果也与使用基于Navier-Stokes公式的端壁损失,轮廓损失的相关性以及假设湍流扩散的简单径向混合模型的“经典”通流方法获得的结果进行了比较。

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