摘要
在超声速流动中,激波与湍流结构的相互作用会产生高强度的激波噪声.激波噪声的高保真计算要求激波捕捉格式具有高阶精度、低耗散和低色散特性,同时还要尽可能地减弱格式的非线性效应.现有的六阶精度迎风/对称混合型加权非线性紧致格式CCSSR-HW-6在基于对称模板构造网格中心处的数值通量时引入了两级加权,且两级加权都需要构造非线性的权系数,因而非线性效应较强.本文以修正波数的误差积分函数为优化目标函数,优化了CCSSR-HW-6格式的非线性特性,建立了加权优化紧致格式WOCS.精度验证表明WOCS格式的精度高于5阶.谱特性分析表明,与原方法相比, WOCS格式的耗散误差和非线性效应显著降低.典型激波噪声问题数值实验表明:WOCS格式不仅提高了对高频波的分辨能力,而且显著地消除了数值解中因格式的非线性效应所导致的非物理振荡.
For the supersonic flow, the shock waves interact with the turbulent structures to generate high intensity shock-associated noise. High fidelity numerical simulation of shock-associated noise requires the shock-capturing scheme to have the properties of high-order accuracy, low dissipation and low dispersion. It is also necessary to reduce the nonlinear effect caused by the nonlinear implementation of scheme as much as possible. The existing upwind/symmetric hybrid weighted non-linear compact scheme with sixth order accuracy(called by CCSSR-HW-6 scheme, Journal of Computational Physics, 2015, 284: 133-154) introduces two-stage weighting strategy to construct the numerical flux at the cell center based on the symmetric stencil. Each stage of weighting in CCSSR-HW-6 scheme must design a nonlinear function for the weighting coefficient, which makes the nonlinear effect enhanced. In this paper, a weighted optimization compact scheme(called by WOCS scheme) is established through optimizing the nonlinear characteristics of original CCSSR-HW-6 scheme. The error integral function of modified wavenumber is chosen as the optimization objective function. The accuracy verification shows that the WOCS scheme has more than fifth order accuracy. The analysis of spectral property shows that compared to original CCSSR-HW-6 scheme, the dissipation error and the nonlinear effect of WOCS scheme are significantly reduced. Numerical experiments on several typical shock-associated noise problems show that the WOCS scheme not only improves the resolving ability of high-frequency waves, but also significantly attenuates the non-physical oscillations in numerical solution caused by the nonlinear effect.
作者
李虎
罗勇
刘旭亮
武从海
韩帅斌
王益民
Li Hu;Luo Yong;Liu Xuliang;Wu Conghai;Han Shuaibin;Wang Yimin(State Key Laboratory of Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,Sichuan,China;Computational Aerodynamics Institute,China Aerodynamics Research and Development center,Mianyang 621000,Sichuan,China)
出处
《力学学报》
EI
CAS
CSCD
北大核心
2022年第10期2747-2759,I0003,共14页
Chinese Journal of Theoretical and Applied Mechanics
基金
国家自然科学基金(11732016,11972360,12172374,12102450)
四川省科技计划(2018JZ0076)
中国空气动力研究与发展中心基础和前沿技术研究基金(PJD20200185)
国家数值风洞工程资助项目。
关键词
激波噪声
激波捕捉格式
紧致格式
非线性效应
shock-associated noise
shock-capturing scheme
compact scheme
nonlinear effect