A WEIGHTED-OPTIMIZATION COMPACT SCHEME FOR SHOCK-ASSOCIATED NOISE COMPUTATION AND ITS NONLINEAR EFFECT ANALYSIS

被引:0
|
作者
Li H. [1 ]
Luo Y. [1 ]
Liu X. [1 ]
Wu C. [1 ]
Han S. [1 ]
Wang Y. [1 ]
机构
[1] 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
关键词
compact scheme; nonlinear effect; shock-associated noise; shock-capturing scheme;
D O I
10.6052/0459-1879-22-254
中图分类号
学科分类号
摘要
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. © 2022 Chinese Journal of Theoretical and Applied Mechanics Press. All rights reserved.
引用
收藏
页码:2747 / 2759
页数:12
相关论文
共 35 条
  • [1] Colonius T, Lele SK., Computational aeroacoustics: progress on nonlinear problems of sound generation, Progress in Aerospace Sciences, 40, pp. 345-416, (2004)
  • [2] Tam CKW., Recent advances in computational aeroacoustics, Fluid Dynamics Research, 38, pp. 591-615, (2006)
  • [3] Liu XD, Osher S, Chan T., Weighted essentially non-oscillatory schemes, Journal of Computational Physics, 115, pp. 200-212, (1994)
  • [4] Jiang GS, Shu CW., Efficient implementation of weighted eno schemes, Journal of Computational Physics, 126, pp. 202-228, (1996)
  • [5] Zhang SH, Zhang HX, Shu CW., Topological structure of shock induced vortex breakdown, Journal of Fluid Mechanics, 639, pp. 343-372, (2009)
  • [6] Zhang SH, Zhang YT, Shu CW., Multistage interaction of a shock wave and a strong vortex, Physics of Fluids, 17, (2005)
  • [7] Li Hu, Luo Yong, Han Shuaibin, Et al., Numerical study on the generation position of screech tone in axisymmetric supersonic jet based on modal decomposition, Chinese Journal of Theoretical and Applied Mechanics, 54, 4, pp. 978-993, (2022)
  • [8] Li Hu, Zhang Shuhai, Direct numerical simulation of decaying compressible isotropic turbulence, Chinese Journal of Theoretical and Applied Mechanics, 44, 4, pp. 673-686, (2012)
  • [9] Liu Xuliang, Zhang Shuhai, Direct numerical simulation of the interaction of 2 D shock wave and shear layer, Chinese Journal of Theoretical and Applied Mechanics, 45, 1, pp. 61-75, (2013)
  • [10] Henrick AK, Aslam TD, Powers JM., Mapped weighted essentially non-oscillatory schemes: Achieving optimal order near critical points, Journal of Computational Physics, 207, pp. 542-567, (2005)