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Vorticity Confinement Technique for Preservation of Tip Vortex of Rotating Blade

机译:保留旋转叶片尖端涡旋的涡度限制技术

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In this study the Vorticity Confinement (VC) approach is combined with Total Variation Diminishing (TVD) technique to avoid over-confinement and divergence of upwind second-order of approximation schemes. The TVD schemes were combined with the first (constant confinement parameter ε) and second (constant unit-less confinement parameter c) VC formulations and to adoptive vorticity confinement formulation by Hahn and laccarino. These VC techniques were applied to convected Taylor vortex. For the former two VC methods combination of the second-order upwind discretization scheme with VC shows significant over-confinement of convected vortex whereas the first-order discretization scheme leads to strong dissipation of vortex. While the latter VC technique shows acceptable results for first-order upwind scheme, it either diverges or strongly over-confines when the second-order upwind discretization scheme is adopted. The combination of VC with TVD shows flowfield close to analytical convected vortex for above listed VC methods. The proposed combined TVD and VC technique is applied to tip vortex generated by rotating blade and compared to experiment. The optimum value of vorticity confinement parameter is adjusted to these conditions. The grid generation issues and needed local grid refinement are discussed. Convergence of CFD algorithm with added vorticity confinement is confirmed. Application of VC to CFD code FLUENT shows much more close comparison to experimental results in terms of vortex velocity profile and size of vortex core compared to the same CFD code without VC approach.
机译:在这项研究中,涡度约束(VC)方法与总变化量递减(TVD)技术相结合,以避免过度约束和迎风二阶逼近方案的发散。 TVD方案与第一个(恒定约束参数ε)和第二个(恒定的无单元约束参数c)VC公式结合,并由Hahn和laccarino应用于过继涡度约束公式。这些VC技术应用于对流泰勒涡旋。对于前两种VC方法,二阶迎风离散化方案与VC的组合显示出对流涡旋的显着过度约束,而一阶离散化方案导致涡流的强烈消散。虽然后者的VC技术对于一阶迎风方案显示了可接受的结果,但是当采用二阶迎风离散化方案时,它要么发散,要么过度过度集中。 VC与TVD的结合显示了上述VC方法的流场接近解析对流涡流。提出的TVD和VC组合技术应用于旋转叶片产生的叶尖涡流,并与实验进行了比较。将涡度限制参数的最佳值调整为这些条件。讨论了网格生成问题和所需的局部网格优化。证实了CFD算法在增加涡度约束下的收敛性。与没有VC方法的相同CFD代码相比,将VC应用于CFD代码FLUENT表现出与实验结果更接近的涡流速度分布和涡流核尺寸。

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