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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >On the definition of the secondary flow in three-dimensional cascades
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On the definition of the secondary flow in three-dimensional cascades

机译:关于三维级联中二次流的定义

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The present article proposes a novel methodology to evaluate secondary flows generated by the annulus boundary layers in complex cascades. Unlike two-dimensional (2D) linear cascades, where the reference flow is commonly defined as that measured at midspan, the problem of the reference flow definition for annular or complex 3D linear cascades does not have a general solution up to the present time. The proposed approach supports secondary flow analysis whenever exit streamwise vorticity produced by inlet endwall boundary layers is of interest. The idea is to compute the reference flow by applying slip boundary conditions at the endwalls in a viscous 3D numerical simulation, in which uniform total pressure is prescribed at the inlet. Thus the reference flow keeps the 3D nature of the actual flow except for the contribution of the endwall boundary layer vorticity. The resulting secondary field is then derived by projecting the 3D flow field (obtained from both an experiment and a fully viscous simulation) along the local reference flow direction; this approach can be proficiently applied to any complex geometry. This method allows the representation of secondary velocity vectors with a better estimation of the vortex extension, since it offers the opportunity to visualize also the region of the vortices, which can be approximated as a potential type. Furthermore, a proficient evaluation of the secondary vorticity and deviation angle effectively induced by the annulus boundary layer is possible. The approach was preliminarily verified against experimental data in linear cascades characterized by cylindrical blades, not reported for the sake of brevity, showing a very good agreement with the standard methodology based only on the experimental midspan flow field. This article presents secondary flows obtained by the application of the proposed methodology on two annular cascades with cylindrical and 3D-designed blades, stressing the differences with other definitions. Both numerical and experimental results are considered. [PUBLICATION ABSTRACT]
机译:本文提出了一种新颖的方法来评估复杂级联中由环空边界层产生的二次流。与通常将参考流定义为在中跨测量的二维(2D)线性级联不同,环形或复杂3D线性级联的参考流定义问题一直没有解决。只要感兴趣的是入口端壁边界层产生的出口流向涡流,建议的方法就可以支持二次流分析。该想法是通过在粘性3D数值模拟中在端壁处应用滑移边界条件来计算参考流量,其中在入口处规定了均匀的总压力。因此,除了端壁边界层涡度的贡献之外,参考流保持实际流的3D性质。然后,通过沿局部参考流向投影3D流场(从实验和完全粘性仿真中获得)来导出生成的次级场。这种方法可以熟练地应用于任何复杂的几何体。该方法可以更好地估计涡旋延伸,从而表示次要速度矢量,因为它提供了可视化涡旋区域的机会,该区域可以近似为潜在类型。此外,可以有效评估由环边界层有效引起的二次涡度和偏角。该方法已针对具有圆柱叶片特征的线性叶栅中的实验数据进行了初步验证,为简洁起见未进行报道,表明该方法与仅基于实验中跨流场的标准方法具有很好的一致性。本文介绍了通过将所提出的方法应用于带有圆柱和3D设计叶片的两个环形叶栅上而获得的二次流,并强调了与其他定义的区别。数值和实验结果都被考虑。 [出版物摘要]

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