期刊文献+

一种求解欧拉方程的高精度数值格式

A high accuracy numerical scheme for solving Euler equation
下载PDF
导出
摘要 为了优化加权本质无振荡(weighted essentially non-oscillatory,WENO)格式在流体力学中的计算性能,在WENO-JS格式和WENO-M格式加权方法研究分析的基础上,基于广义不可分差分算子推导出新局部光滑因子,构造出WENO-NS格式。将总能对流迎风和分压(E-CUSP)格式与七阶WENO-NS格式耦合得到新格式。在空间层上,采用七阶WENO-NS格式重构低耗散E-CUSP格式中的通量;在时间层上,采用四阶总变差递减的龙格-库塔(total variation decreasing Runge-Kutta,TVD-Runge-Kutta)方法推进,对一维激波管问题进行了数值模拟。观察可得,耦合的E-CUSP-WENO-NS7对接触间断和激波的捕捉更为精确。结果分析表明,耦合的新格式可以更陡峭地捕捉到激波,计算结果精度高,稳定性能好。 In order to optimize the computational performance of weighted essentially non-oscillatory(WENO)scheme in hydrodynamics,on the basis of the research and analysis of the weighted methods of WENO-JS scheme and WENO-M scheme,a new local smoothness indicator is obtained from the generalized undivided difference operator,and the WENO-NS scheme is constructed.The new scheme is obtained by coupling the total energy convective upwind and split pressure schemes(E-CUSP)with the seventh-order WENO-NS scheme.In the space layer,the flux in the low dissipation E-CUSP scheme is reconstructed by the seventh-order WENO-NS scheme,and in the time layer,the fourth-order total variation decreasing Runge-Kutta(TVD-Runge-Kutta)method is used to simulate the one-dimensional shock tube problem.It can be observed that the coupled E-CUSP-WENO-NS7 is more accurate in capturing contact discontinuities and shock waves.The results show that the new coupled scheme can capture shock waves more steeply,and the calculation results are of high accuracy and good stability.
作者 任琴琴 白晓雅 郑秋亚 梁益华 REN Qinqin;BAI Xiaoya;ZHENG Qiuya;LIANG Yihua(School of Science,Chang’an University,Xi’an 710064,China;Aeronautical Laboratory of Computational Fluid Dynamics,Aeronautics Computing Technique Research Institute,Xi’an 710068,China)
出处 《合肥工业大学学报(自然科学版)》 CAS 北大核心 2021年第4期569-576,共8页 Journal of Hefei University of Technology:Natural Science
基金 航空科学基金资助项目(2015ZA31002)。
关键词 欧拉方程 总能对流迎风和分压(E-CUSP)格式 WENO-NS格式 光滑因子 高精度 Euler equation total energy convective upwind and split pressure schemes(E-CUSP) WENO-NS scheme smoothness indicator high accuracy
  • 相关文献

参考文献3

二级参考文献44

  • 1Steger J L, Warming R F. Flux vector splitting of the inviscid gas dynamics equations with application to finite difference schemes [ J ]. Journal of Computational Physics, 1981, 40 (2) : 263 - 293.
  • 2Van Leer B. Flux vector splitting for Euler equations [ C ]//Eighth International Conference on Numerical Methods in Fluid Dynamics, Berlin: Lecture Notes in Physics, 1982: 170.
  • 3Hanel D, Schwane R, Seider G. On the accuracy of upwind schemes for the solution of the Navier-Stokes equations [ R]. AIAA - 1987 - 1105.
  • 4Hanel D, Schwane R. An implicit flux-vector splitting scheme for the computation of viscous hypersonic flow [ R]. A1AA - 1989 - 0274.
  • 5Coirier W J, Van Leer B. Numerical flux formulas for the Euler and Navier-Stokes equations: lI. Progress in flux-vector splitting [ R]. AIAA - 1991 - 1566.
  • 6Roe P L. Approximate Riemann solvers, parameter vectors and difference schemes [ J]. Journal of Computational Physics, 1981, 43 : 357 - 372.
  • 7Osher S, Solomon F. Upwind difference schemes for hyperbolic conservation laws [ J]. Mathematical computations, 1982, 158 : 339 - 374.
  • 8Toro E F, Spruce M, Speares W. Restoration of the contact surface in the HLL-Riemann solver [ J]. Shock Waves, 1994, 4 : 25 - 34.
  • 9Peery K M, Imlay S T. Blunt-body flow simulations [R]. AIAA -1988 -2904.
  • 10Quirk J J. A contribution to the great Riemann solver debate [ R]. ICASE Report, 1992 -64.

共引文献11

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部