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Transition to turbulence in the separated shear layers of yawed circular cylinders

机译:在偏航圆柱体的分离剪切层中过渡到湍流

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Spatial and temporal resolution of transition to turbulence inside the free-shear layers of two yawed circular cylinders is the subject of the present investigation. These physics were resolved using the large-eddy simulation (LES) methodology. An O-type grid was implemented such that the spatial scales of the LES computation fully resolved the energy range physics of the shear layers at Reynolds number Re_D = 8000 based on the cylinder diameter. The two test cases modeled the cylinder span skewed at angles 45° and 60° from the horizontal axis. Observations revealed the same transition process as the normal cross-flow state. Soon after separation, Tollmien-Schlichting disturbances were predicted that evolved into Kelvin-Helmholtz (K-H) eddies before absorption by the large-scale Karman-type vortices. These eddies defaulted to a spanwise wavy pattern similar to a normal cross-flow due to their three-dimensional instability. No mixed modes were found between the K-H (Bloor) and Strouhal frequencies. The effect of yaw angle shortened the transition process. As a result, peak turbulence levels inside the wake formation zone approach the downstream cylinder periphery. In addition, the dimensionless frequencies of the K-H eddies lie above the normal cross-flow relationship as formulated by Bloor (1964). Disparity between the yawed and normal cross-flow states was further emphasized by the shear-layer transition characteristics. Although each property displayed the expected exponential growth during transition to turbulence, their dimensionless form was miss-aligned with those of the normal cross-flow case. Based on the present evidence, additional simulations (and/or experimental measurements) are necessary to form conclusive arguments regarding the expected behavior of the transition characteristics within the free-shear layers of yawed circular cylinders.
机译:在两个偏航圆柱体的自由剪切层内部过渡到湍流的时空分辨率是本研究的主题。这些物理学是使用大涡模拟(LES)方法解决的。实施了O型网格,以使LES计算的空间尺度完全基于圆柱体直径解决了雷诺数Re_D = 8000时剪切层的能量范围物理学。这两个测试案例对与水平轴倾斜45°和60°的圆柱跨度进行了建模。观察结果显示出与正常错流状态相同的过渡过程。分离后不久,预计Tollmien-Schlichting扰动会演变成开尔文-亥姆霍兹(K-H)涡流,然后被大规模的卡曼型涡旋吸收。由于它们的三维不稳定性,这些涡流默认为类似于正常横流的展向波浪形图案。在K-H(布鲁尔)频率和Strouhal频率之间未发现混合模式。偏航角的影响缩短了过渡过程。结果,尾流形成区域内的峰值湍流水平接近下游的汽缸外围。此外,K-H涡流的无量纲频率高于Bloor(1964)提出的正常横流关系。剪切层过渡特征进一步强调了偏航和正常横流状态之间的差异。尽管每个属性在过渡到湍流过程中都显示出预期的指数增长,但它们的无量纲形式与常规横流情况没有对齐。基于目前的证据,需要额外的模拟(和/或实验测量)来形成关于偏航圆柱体自由剪切层内过渡特性预期行为的结论性论据。

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