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DEVELOPMENT AND VALIDATION OF A COMPRESSIBLE LARGE-EDDY SIMULATION CODE WITH OVERSET MESH METHOD

机译:可逆网格法的可压缩大涡模拟代码开发与验证

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This paper describes basic ideas for the design of a new computational fluid dynamics (CFD) code for large-eddy simulation (LES), as well as presenting fundamental validation and demonstration cases. The developed code combines high-order structured solver with overset mesh technique, which enables to control mesh density easily with keeping high mesh quality. The validations were conducted over two different flow regimes. The mesh size criteria for the present code were identified from the systematic mesh study of wall-bounded channel flow. In addition, the wake profile after the circular cylinder as a validation of free shear flow showed good agreement with the reference data. Then the validated code was applied to the flow field of highly loaded stator vane. The developed solver reproduced the position of separation bubble accurately however, the velocity profiles on the vane needed improvement by introducing free stream turbulence. From the sequence of validation and application studies, it was concluded that the present code can be used for the researches of fundamental turbulent flow field in turbomachinery.
机译:本文介绍了用于大涡模拟(LES)的新计算流体动力学(CFD)代码设计的基本思想,并介绍了基本的验证和演示案例。开发的代码将高阶结构化求解器与过剩网格技术相结合,可以轻松控制网格密度并保持高网格质量。验证是在两种不同的流态下进行的。本代码的网格大小标准是通过对有边界的通道流动进行系统的网格研究确定的。此外,作为自由剪切流的验证,圆柱后的尾流曲线与参考数据显示出良好的一致性。然后将经过验证的代码应用于高负荷定子叶片的流场。开发的求解器可以精确地再现分离气泡的位置,但是,需要通过引入自由流湍流来改善叶片上的速度分布。从验证和应用研究的顺序来看,可以得出结论,该代码可用于涡轮机械基础湍流场的研究。

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