一种用于间断装配的流场结构辨识算法

刘君; 陈泽栋; 陈洁; 邹东阳

doi:10.7638/kqdlxxb-2017.0212

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一种用于间断装配的流场结构辨识算法

研究论文 | 更新时间：2026-05-28

- 一种用于间断装配的流场结构辨识算法
- A surface extraction method of flow feature for shock-fitting scheme
- 空气动力学学报 2019年37卷第3期页码：373-381
- 作者机构：
  
  1. 大连理工大学航空航天学院,大连,116024
  2. 大连理工大学工程力学系,大连,116024
- 作者简介：
  
  刘君(1965-), 男, 博士, 教授, 研究方向:计算流体力学, 空气动力学.E-mail:liujun65@dlut.edu.cn
- 基金信息：
  
  国家自然科学基金(11872144, 11532016)
- DOI：10.7638/kqdlxxb-2017.0212
  中图分类号： V211.3
- 纸质出版：2019
- 稿件说明：
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刘君, 陈泽栋, 陈洁, 邹东阳. 一种用于间断装配的流场结构辨识算法[J]. 空气动力学学报, 2019, 37(3): 373-381.

LIU Jun, CHEN Zedong, CHEN Jie, et al. A surface extraction method of flow feature for shock-fitting scheme[J]. 2019, 37(3): 373-381.
刘君, 陈泽栋, 陈洁, 邹东阳. 一种用于间断装配的流场结构辨识算法[J]. 空气动力学学报, 2019, 37(3): 373-381. DOI： 10.7638/kqdlxxb-2017.0212.

LIU Jun, CHEN Zedong, CHEN Jie, et al. A surface extraction method of flow feature for shock-fitting scheme[J]. 2019, 37(3): 373-381. DOI： 10.7638/kqdlxxb-2017.0212.

摘要

使用激波装配法时，初始激波是否准确将会对计算过程产生影响。为了确定初始激波的位置，提出了一种新的流场结构辨识算法。该算法以捕捉法计算得到的流场作为系统观测数据，根据密度、压力等参数从该数据中获取激波和接触间断等流动特征周围的网格节点作为离散点集。通过将该离散点集分割成若干子区域，在各子区域内进行分片拟合，最终将离散点集拟合成连续光滑的实体模型，并将此作为初始激波面。在二维方法的基础上，通过引入单位球模型成功将该辨识算法拓展到三维应用。结果表明，采用该方法获得的间断曲面（激波和接触间断）与捕捉法流场中的间断分布吻合较好，作为初始间断面用于装配法可快速得到收敛解。该方法解决了应用激波装配法时确定初始间断面的难题。此外，该方法还可用于网格自适应方法。选择不同流动参数，可以获得相应流场特征结构的空间曲面，在此曲面的基础上可进行网格局部加密或重剖分。该流场结构辨识算法用于网格自适应具有网格尺度自由设置的优势。

Abstract

A new surface extraction method named source-rays method is proposed to locate and shape initial shock wave surface for shock-fitting algorithms. In this method

the flow field data acquired by the shock-capturing schemes are used as the observed data

and the grid nodes with the features such as shock waves and contact discontinuities are obtained as a discrete point set according to the parameters of density

pressure and others. The discrete point set is finally assembled into a continuous smooth surface by being segmented into several subsets for fragment fitting. Based on the two-dimensional method

this identification algorithm is extended to three-dimensional application by introducing a unit sphere model. The discrete points are fitted to a series of triangular patches with determined connection relationship by a unit sphere

and a smooth continuous surface can be assembled. The results show that the feature surface (shock wave and contact discontinuity) obtained by the source-rays method coincides with the discontinuous distribution in the flow field calculated by the shock-capturing schemes. By using the extracted feature surface as the initial shock wave surface

the convergence solution can be quickly obtained in shock-fitting algorithm. In addition

this method can also be used in the adaptive mesh refinement procedure. According to different flow parameters

the spatial surfaces of the corresponding flow field structures can be obtained. Based on these surfaces

the mesh grid can be locally refined. This flow field feature surface extraction method has the advantage of grid scale set arbitrarily for mesh adaptation procedure.

关键词

Keywords

references

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