主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司
邹东阳, 陈泽栋, 常思源, 等. 基于特征线理论的辨识法在激波装配中的应用[J]. 气体物理, 2018, 3(1): 41-49. DOI: 10.19527/j.cnki.2096-1642.2018.01.006
引用本文: 邹东阳, 陈泽栋, 常思源, 等. 基于特征线理论的辨识法在激波装配中的应用[J]. 气体物理, 2018, 3(1): 41-49. DOI: 10.19527/j.cnki.2096-1642.2018.01.006
ZOU Dong-yang, CHEN Ze-dong, CHANG Si-yuan, et al. A Shock Detection Method Based on the Theory of Characteristics and its Application in Shock-Fitting Methods[J]. PHYSICS OF GASES, 2018, 3(1): 41-49. DOI: 10.19527/j.cnki.2096-1642.2018.01.006
Citation: ZOU Dong-yang, CHEN Ze-dong, CHANG Si-yuan, et al. A Shock Detection Method Based on the Theory of Characteristics and its Application in Shock-Fitting Methods[J]. PHYSICS OF GASES, 2018, 3(1): 41-49. DOI: 10.19527/j.cnki.2096-1642.2018.01.006

基于特征线理论的辨识法在激波装配中的应用

A Shock Detection Method Based on the Theory of Characteristics and its Application in Shock-Fitting Methods

  • 摘要: 准确地给出激波位置信息对于激波装配极为重要.但是,在使用计算流体力学(computational fluid dyna-mics,CFD)方法模拟复杂流动时很难准确地给出激波的位置.根据激波捕捉得到的流场信息确定的激波位置往往带有极大误差,在定常问题的模拟中,这种误差可以随着迭代逐渐消除,然而在非定常问题的模拟中,这种误差往往会积累甚至导致计算崩溃.文章将基于特征线理论的激波辨识技术应用到激波装配中,根据已有流场信息准确判断激波的位置.对于定常问题,该方法的应用加速了收敛速度;对于非定常问题,该方法的应用可以极大地避免初始误差的产生.

     

    Abstract: It is very important to detect shock positions for a shock-fitting technique. However, it is difficult to get the exact position from the computational results. Numerical errors caused by captured methods usually lead to deflections of shock wave positions. In a steady flow, the deflected errors will be eliminated by iterations. In an unsteady flow, however, the deflected errors may be accumulated and led to wrong results. In the present work, a shock detection method based on the theory of characteristics was used to detect shock positions in shock-fitting techniques. This method is proved to be with good performance both in steady flows and unsteady flows.

     

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