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Isogeometric Boundary Element Analysis of steady incompressible viscous flow, Part 1: Plane problems

机译:稳态不可压缩粘性流动的等几何边界元分析,第1部分:平面问题

摘要

A novel approach is presented to the Boundary Element analysis of steady incompressible flow. NURBS basis functions are used for describing the geometry of the problem and for approximating the unknowns. In addition, the arising volume integrals are treated differently to published work, that is, volumes are described by bounding NURBS curves instead of cells and a mapping is used. The advantage of our approach is that non-trivial boundary shapes can be described with very few parameters and that no generation of cells is required. For the solution of the non-linear equations both classical and modified Newtonâu80u93Raphson methods are used. A comparison of the two methods is made on the classical example of a forced cavity flow, where accurate solutions are available in the literature. The results obtained agree well with published ones for moderate Reynolds numbers using both methods, but it is found that the latter requires a relaxation scheme and considerably more iterations to converge. Finally, it is shown on a practical example of an airfoil how more complex boundary shapes can be approximated with few parameters and a solution obtained with a small number of unknowns.
机译:提出了一种新的方法,用于稳态不可压缩流的边界元分析。 NURBS基本函数用于描述问题的几何形状和近似未知数。此外,对产生的体积积分的处理与已发表的工作有所不同,也就是说,通过限制NURBS曲线而不是像元来描述体积,并使用映射。我们方法的优点是可以用很少的参数来描述非平凡的边界形状,并且不需要生成像元。对于非线性方程的求解,既使用经典方法又使用改进的Newtonâu80u93Raphson方法。两种方法的比较是在强迫腔流的经典示例中进行的,在文献中可以找到准确的解决方案。使用这两种方法,获得的结果与中等雷诺数的已发布结果非常吻合,但是发现后者需要一种松弛方案,并且需要更多的迭代才能收敛。最后,在机翼的一个实际示例中显示了如何用很少的参数和更少量的未知数就能获得更复杂的边界形状。

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