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WENO型有限体积格式高超声速数值激波稳定性分析

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高阶格式在提高计算精度、刻画流动细节等方面具有巨大优势,然而在模拟多维强激波时,高阶格式通常会产生激波失稳问题,制约了其在超声速/高超声速流动模拟中的应用.本文针对加权基本无振荡格式(WENO)型有限体积格式,建立了矩阵稳定性分析方法,为定量分析高阶格式捕捉强激波的稳定性提供了有效工具.利用矩阵稳定性分析方法,对三阶WENO型有限体积格式的激波失稳问题进行定量研究.结果表明,与一阶格式相比,三阶格式面临更严峻的激波失稳问题.在空间三阶精度下,解算器的性质与激波强度是影响数值格式激波稳定性的重要因素.此外,对数值激波失稳的空间位置进行了研究,发现激波失稳源于数值激波结构内部,因此激波结构内部的中间状态是影响格式捕捉强激波稳定性的关键因素.本文为分析三阶WENO型有限体积格式的激波失稳问题提供了有效方法,并对三阶格式数值激波失稳问题的内在机理进行研究,为更深入地理解高阶格式激波失稳问题的内在机理,发展强稳定的高阶格式奠定了基础.
Stability Analysis on the Hypersonic Numerical Shocks for Finite-volume WENO Schemes
High-order schemes offer significant advantages in improving computational accuracy and capturing flow details.However,when simulating multidimensional strong shocks,high-order schemes often suffer shock instability problems,which limit their applications in supersonic/hypersonic flow simulations.In the current study,the matrix stability analysis method is established to quantitatively analyze the stability of the third-order WENO finite-volume scheme in capturing strong shocks.And by using the matrix stability analysis method,the shock instability problem of the third-order scheme is studied.Results indicate that compared with first-order schemes,the third-order scheme has more severe shock instability problems.Under spatial third-order accuracy,the properties of Riemann solvers significantly affect the shock instability problem.Low-dissipative solvers,such as Roe,often lead to shock instability,while the third-order scheme can capture strong shocks when high-dissipation solvers are employed.Furthermore,it has been demonstrated that the intensity of the shock is positively correlated with the shock instability problem,but its impact weakens or even disappears beyond a certain level.Additionally,the spatial location of numerical shock instability is investigated in the current work,and it is found that for the third-order scheme,the shock instability originates from the numerical shock structure.As a result,the intermediate states inside the shock structure are crucial factors affecting the stability of the scheme in capturing strong shocks.When the intermediate states inside the shock structure are closer to the downstream states,the computation will be more stable.This paper provides an effective method for analyzing the shock instability problem of third-order WENO finite-volume schemes and investigates the underlying mechanisms of shock instability problem for the third-order scheme,laying a foundation for further understanding the inherent mechanisms of shock instability problems in high-order schemes and developing stable high-order schemes.

finite-volume methodThird-order WENOhypersonicshock instabilitymatrix stability analysis

任伟杰、谢文佳、张烨、于航、李桦、田正雨

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国防科技大学 空天科学学院,湖南 长沙 410073

有限体积方法 三阶WENO 高超声速 数值激波失稳 矩阵稳定性分析

2024

气动研究与试验

气动研究与试验

ISSN:
年,卷(期):2024.2(1)
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