调整轴向奇异点法以精确计算轴对称体的势流

IF 1.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE
M. F. Zedan
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引用次数: 1

摘要

通过精心挑选的试验用例,系统地研究了轴线奇异性方法在不同解参数下的性能。结果表明,增加单元数和使用拉伸节点分布可以提高求解精度,直到矩阵接近奇异。矩阵条件数随这些参数的增大而增大,且随强度变化的先后顺序和型材厚度的增大而增大。对于中等细度比,线性方法优于零阶方法。当控制点位于节点的x位置时,线性双线方法的效果最好,而当控制点位于节点之间的中间位置时,源方法的效果最好。该双重方法具有比源方法低一个数量级的条件数,并且通常提供更准确的结果并处理更大范围的物体。在适当的解参数下,该方法对无坡面不连续体具有较好的精度。Hemsch最近提出的平滑技术已被证明可以减少矩阵的条件数;然而,它应该谨慎使用。建议仅在溶液具有近似奇异矩阵的高度振荡时使用它。提出了平滑参数最优值的判据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Tuning the axial singularity method for accurate calculation of potential flow around axisymmetric bodies
Abstract The performance of axial line singularity methods has been investigated systematically for various solution parameters using carefully chosen test cases. The results indicate that increasing the number of elements and using stretched node distribution improves the solution accuracy until the matrix becomes near-singular. The matrix condition number increases with these parameters as well as with the order of intensity variation and profile thickness. For moderate fineness ratios, the linear methods outperform zero-order methods. The linear doublet method performs best with control points at the x-locations of nodes while the source methods perform best with control points mid-way between nodes. The doublet method has a condition number an order of magnitude lower than the source method and generally provides more accurate results and handles a wider range of bodies. With appropriate solution parameters, the method provides excellent accuracy for bodies without slope discontinuity. The smoothing technique proposed recently by Hemsch has been shown to reduce the condition number of the matrix; however it should be used with caution. It is recommended to use it only when the solution is highly oscillatory with a near-singular matrix. A criterion for the optimum value of the smoothing parameter is proposed.
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来源期刊
Aeronautical Journal
Aeronautical Journal 工程技术-工程:宇航
CiteScore
3.70
自引率
14.30%
发文量
86
审稿时长
6-12 weeks
期刊介绍: The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.
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