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Construction of conservative finite difference schemes suitable for simulations of turbulent flows with complicated geometry and application to wind turbine aerodynamics

机译:保守有限差分方案的构建,适用于复杂几何形状的湍流流动模拟及风力涡轮机空气动力学

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摘要

In order to conduct direct numerical simulation (DNS) or large eddy simulation (LES) of turbulent flows with complicated geometry, we have to use accurate finite difference methods in generalized curvilinear coordinate system. In this report, finite difference schemes (FDSs) in generalized curvilinear coordinate system suitable for simulations of incompressible turbulent flow are constructed by relatively simple extension of the proper finite difference schemes derived in equidistant Cartesian coordinate system. Preliminary tests by DNSs of a plane channel flow reveal that the mesh dependency such as non-orthogonality and non-uniformity on results is reduced by the present FDS. As application of the FDS to wind turbine aerodynamics, large eddy simulations of flow fields around a circular cylinder and an airfoil section for wind turbines are simulated using HITACHI SR8000 supercomputer installed at the Tsukuba Advanced Computing Center (TACC) of Agency of Industrial Science and Technology (AIST). The formation of laminar separation bubbles with reverse flow region on wind turbine blades are successfully reproduced in our simulation.
机译:为了通过复杂的几何进行直接数值模拟(DNS)或大型涡流模拟(LES),我们必须在广义曲线坐标系中使用精确的有限差分方法。在本报告中,通过相对简单地延长等距笛卡尔坐标系衍生的适当有限差分方案的相对简单的延伸构成了适用于不可压缩湍流的一般曲线坐标系中的有限差分方案(FDS)。平面通道流的DNSS的初步测试表明,目前的FDS减少了诸如非正交性和不均匀性的网格依赖性。作为FDS在风力涡轮机空气动力学的应用,使用安装在工业科学和技术机构的Tsukuba高级计算中心(TACC)的日立SR8000超级计算机围绕圆筒围绕圆柱体的流场和风力涡轮机的翼型部分的大涡流模拟(辅助)。在我们的模拟中成功地再现了风力涡轮机叶片上具有反向流动区域的层间分离气泡的形成。

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