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THEORETICAL AND EXPERIMENTAL STUDY ON FLUID FLOW IN VALVE CHANNELS PART II - PRESSURE LOSS DATA

机译:阀通道中流体流体的理论与实验研究 - 压力损耗数据

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As previously pointed out frictionless incompressible jet flow(with separation at sharp edges) is essential to the present issues, appropriate data have been collected and produced by the author. These data are partly based on theoretical jet flow solutions partly on experimental results which have been gained with sufficiently thin boundary layers. In some cases pressure recovery according to momentum theorem(sudden enlargement) is included in these data. All the data taken from literature were checked carefully and had to he intensely processed to fit into the required context. Data based on theoretical jet flow solutions are marked by "Th", data based on experiments by "Ex". The latter are expected to be within a ±10% margin to the theoretical jet flow solution (not yet available in literature to the knowledge of the author). Data which include calculated pressure recovery(by momentum theorem) is marked by "Mo". In special cases data on force coefficients are also presented.
机译:如前所述,摩擦不可压缩的射流(在尖锐边缘处分离)对当前问题至关重要,所以通过作者收集和生产适当的数据。这些数据部分基于部分地基于理论射流解决方案,这些方法部分地基于已经用足够薄的边界层获得的实验结果。在一些情况下,根据动量定理(突然放大)包括在这些数据中的压力恢复。仔细检查从文献中取出的所有数据,不得不紧张地处理以适应所需的背景。基于理论喷射流程解决方案的数据标有“TH”,基于“EX”的实验数据。后者预计将在理论射流解决方案的余量范围内(文献中尚未提供给作者的知识)。包括计算压力恢复(按动量定理)的数据标有“Mo”。在特殊情况下,还提出了关于力系数的数据。

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