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COMPUTATIONAL STUDY OF KELVIN-HELMHOLTZ INSTABILITY CREATED BY INTERACTION OF THE MAINSTREAM FLOW AND THE SEAL FLOW IN GAS TURBINES

机译:燃气轮机主干流与密封流相互作用产生开尔文-赫尔默兹失稳的计算研究

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The present paper gives a contribution to a better understanding of the emergence of Kelvin-Helmholtz instabilities (KHI) in gas turbines. In an earlier paper of the authors, the occurrence of the KHI's near the rim cavity of a 1.5 stage gas turbine has been examined by use of CFD methods. It is shown that the KHI's occur, when the swirl component of the hot gas flow is very strong. Due to the fact, that a high swirl is produced by the guide vanes of the first stage, this matter concerns all common gas turbines. In order to get a basic theoretical background of the emergence of the KHI's, 2D CFD investigations of the flow behind a splitter plate have been performed showing the development of KHI's downstream of the splitter plate. To validate the numerical results a comparison to test rig data is used. This shows that the numerical method can simulate the characteristics of the KHI's. Furthermore, a parameter study is conducted to extract parameters describing the appearance of KHI's, the vortex periodicity and stability criteria. The main intention of this paper is to deliver "KHI parameters", which are able to describe the development of the KHI in gas turbine rim cavities.
机译:本文有助于更好地理解燃气轮机中Kelvin-Helmholtz不稳定性(KHI)的出现。在作者的较早论文中,已经通过使用CFD方法检查了1.5级燃气轮机边缘腔附近KHI的发生。结果表明,当热气流的涡旋分量非常强时,会发生KHI。由于这一事实,第一级的导向叶片会产生高涡流,因此,这与所有普通的燃气轮机有关。为了获得KHI的出现的基本理论背景,对分流板后面的流动进行了二维CFD研究,显示了KHI在分流板下游的发展。为了验证数值结果,使用了与试验台数据的比较。这表明数值方法可以模拟KHI的特性。此外,进行了参数研究以提取描述KHI的外观,涡旋周期性和稳定性标准的参数。本文的主要目的是提供“ KHI参数”,这些参数能够描述燃气轮机轮辋腔中KHI的发展。

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