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Experimental and numerical investigations of the effects of incident turbulence on the flow over a surface-mounted prism.

机译:实验和数值研究了湍流对表面安装的棱镜上流动的影响。

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The issue of the effects of free stream turbulence on the flow field over a surface-mounted prism is examined through experimental and numerical investigations. In the experimental studies, particle image velocimetry measurements are conducted in the ESM water tunnel at Reynolds number of 9,600 and under two cases of turbulent inflow conditions. The results show that the mean flow separation, reattachment and parameters such as mean velocity, root mean square, Reynolds stresses and turbulent kinetic energy are affected by the turbulence characteristics of the incident flow. The instantaneous dynamics of the interactions between the separating shear layer and the solid wall and between the shear layer and the turbulence in the incident flow are detailed.; In the numerical studies, large eddy simulations of the flow over a surface-mounted prism under two inflow conditions; namely, smooth inflow and isotropic homogeneous turbulence inflow, are performed. The use of a fifth-order scheme (CUD-II-5), which is a member of a family of Compact Upwind Difference schemes, in large eddy simulations of this flow is assessed. The performance of this scheme is validated by comparing the rate of temporal decay of isotropic turbulence with available experimental measurements for grid-generated turbulence. The results show that the spectra are sensitive to the method of flux vector splitting needed for the implementation of the upwind scheme. With van Leer splitting, the CUD-II-5 scheme is found to be too dissipative. On the other hand, using the Lax-Friedrichs vector splitting yields good agreement with experiments by controlling the level of artificial dissipation. This led us to recommend a new procedure, we denote by C6CUD5 scheme, that combines a compact sixth-order scheme with the CUD-II-5 scheme for large eddy simulation of complex flows. The simulation results, including flow patterns, pressure fields and turbulence statistics show that the CUD-II-5 scheme, with Lax-Friedrichs flux vector splitting; provides high resolution of local flow structures. The results present new physical aspects of the flow topology over surface-mounted prisms. The effects of the incident homogeneous turbulence on the size of the separation region and suction pressures are determined by pointing out differences in the flow topologies between the two incident flow cases.
机译:通过实验和数值研究,研究了自由射流湍流对表面安装棱镜上方流场的影响问题。在实验研究中,在雷诺数为9,600的ESM水隧道中以及在两种湍流条件下对颗粒图像测速仪进行了测量。结果表明,平均流分离,重新附着和平均流速,均方根,雷诺应力和湍动能等参数均受入射流湍流特性的影响。详细介绍了分离剪切层与固体壁之间以及剪切层与湍流之间的相互作用的瞬时动力学。在数值研究中,在两个入流条件下对表面安装棱镜的流动进行了大涡模拟。即,进行平滑流入和各向同性均匀湍流流入。评估了五阶方案(CUD-II-5),该方案是紧凑迎风差异方案系列的成员,并且在该流的大型涡流模拟中进行了评估。通过将各向同性湍流的时间衰减率与可用的网格生成湍流实验测量值进行比较,验证了该方案的性能。结果表明,该频谱对实现迎风方案所需的通量矢量分裂方法很敏感。通过van Leer拆分,发现CUD-II-5方案过于耗散。另一方面,通过控制人工耗散的水平,使用Lax-Friedrichs向量拆分可产生与实验的良好一致性。这导致我们推荐一个新的过程,用C6CUD5方案表示,该方案将紧凑的六阶方案与CUD-II-5方案结合起来,用于复杂流的大涡模拟。包括流型,压力场和湍流统计在内的仿真结果表明,CUD-II-5方案采用Lax-Friedrichs磁通矢量分裂。提供高分辨率的局部流动结构。结果显示了表面安装棱镜上流动拓扑的新物理方面。入射均匀湍流对分离区域的大小和吸气压力的影响是通过指出两种入射流动情况之间流动拓扑的差异来确定的。

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