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Transition Models for Turbomachinery Boundary Layer Flows: A Review

机译:涡轮机械边界层流的过渡模型:综述

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摘要

Current models for transition in turbomachinery boundary layer flows are reviewed. The basic physical mechanisms of transition processes and the way these processes are expressed by model ingredients are discussed. The fundamentals of models are described as far as possible, with a common structure of the equations and with emphasis on the similarities between the models. Tests of models reported in the literature are summarized and our own test is added. A conclusion on the performance of models is formulated.
机译:审查了当前涡轮机边界层流动过渡模型。讨论了过渡过程的基本物理机制以及模型成分表达这些过程的方式。尽可能地描述模型的基本原理,包括方程的通用结构,并强调模型之间的相似性。总结了文献报道的模型测试,并添加了我们自己的测试。提出了关于模型性能的结论。

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