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ZDES and URANS Simulations of 3D Transonic Buffet Over Infinite Swept Wings

机译:无限扫过翅膀的3D跨音速自助式的ZDES和Urans模拟

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This paper presents a study of transonic buffet over three-dimensional infinite swept wings. These configurations consist of the extrusion of an ONERA OALT25 airfoil with periodic boundary conditions in the spanwise direction. Unsteady Reynolds Averaged Navier-Stokes (URANS) simulations are first performed to assess the effect of the sweep angle. Spanwise flow structures are observed on these essentially 2D or 2.5D configurations, forming what has been named buffet cells. The 3D buffet frequency is correlated with the wavelength of these cells and the sweep angle. Then, Zonal Detached Eddy Simulations (ZDES) are carried out over small span and large span wings to provide numerical validation to the URANS simulations. These simulations are used to assess the capacity of hybrid RANS-LES methods to model the 3D effects involved in transonic buffet. At last, these simulations will provide insights into the complex physics involved in transonic buffet.
机译:本文介绍了三维无限扫翅上的跨音速自助式的研究。这些配置包括挤出OnerA oalt25翼型的挤出,其周期方向上的周期边界条件。首先执行不稳定的雷诺斯平均Navier-Stokes(urans)模拟以评估扫描角度的效果。在基本上2D或2.5D配置上观察到翼展的流动结构,形成已被命名的自助细胞。 3D自助频率与这些电池的波长和扫描角度相关。然后,在小跨度和大跨度翼上进行Zonal独立式涡流模拟(ZDES),以提供对尿素模拟的数值验证。这些模拟用于评估混合rans-les方法的容量,以模拟跨音自助式涉及的3D效果。最后,这些模拟将为跨音质自助式涉及的复杂物理提供见解。

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