期刊文献+

无粘可压缩流动的改进高精度方法 被引量:1

One improved high accuracy scheme for compressible inviscid flow computation
下载PDF
导出
摘要 为更准确捕捉复杂流场的流动细节,通过对WENO格式的光滑因子进行改进,发展了一种新的五阶WENO格式。对三阶ENO格式进行加权可以得到五阶WENO格式,但是不同的加权处理,WENO格式在极值处保持加权基本无振荡的效果不同,本文构造了二阶精度的局部光滑因子,及不含一阶二阶导数的高阶全局光滑因子,从而实现WENO格式在极值处有五阶精度。基于改进五阶WENO格式,对一维对流方程、一维和二维可压缩无粘问题进行算例验证,并与传统WENO-JS格式和WENO-Z格式进行比较。计算结果表明,改进五阶WENO格式有较高的精度和收敛速度,有较低的数值耗散,能有效捕捉间断、激波和涡等复杂流动。 For more accurately capturing complex flows,a new fifth-order WENO scheme is developed by improving the smoothing factor of WENO scheme. Weighting the third-order ENO scheme can lead to a fifth-order WENO scheme,but with different weighting methods,the WENO scheme will have different effects of maintaining weighted essentially non-oscillatory schemes at extreme values. In this paper,the local smoothing factor of second-order accuracy and the high-order global smoothing factor without first-order or second-order derivative are constructed,so that the WENO scheme has fifth-order accuracy at the extreme values.Based on the improved fifth-order WENO scheme,the classical problems of one-dimensional convection equations,one-dimensional and two-dimensional Euler equations are verified by examples,and compared with the traditional WENO-JS scheme and WENO-Z scheme.The calculation results show that the improved fifth-order WENO scheme has higher accuracy and convergence speed,and can effectively capture complex flows such as discontinuities,shock waves and eddies with low dissipation.
作者 徐丽 姜明洋 蔡静静 吴硕 XU Li;JIANG Ming-yang;CAI Jing-jing;WU Shuo(School of Mathematics and Physics,Shanghai University of Electric Power,Shanghai 200090,China)
出处 《计算力学学报》 EI CAS CSCD 北大核心 2019年第6期784-791,共8页 Chinese Journal of Computational Mechanics
基金 国家自然科学基金(11502141 11701359)资助项目
关键词 加权本质无振荡 WENO格式 光滑因子 高阶精度 可压缩流动 weighted essentially non-oscillatory WENO scheme smoothness indicators high order accuracy compressible flows
  • 相关文献

参考文献1

二级参考文献16

  • 1He C,Zhao J.Modeling rotor wake dynamics with viscous vortex particle method[J].AIAA Journal,2009, 47 (4):902-915.
  • 2Dietz M,Keler M,Kramer E,et al.Tip vortex conservation on a helicopter main rotor using vortex-adapted chimera grids[J].AIAA Journal,2007, 45 (8):2062-2074.
  • 3Harris R E,Sheta E F,Habchi S D.An Efficient Adaptive Cartesian Vorticity Transport Solver for Rotorcraft Flowfield Analysis[R].AIAA Paper,2010-1072,2010.
  • 4Hariharan N.High Order Accurate Numerical Convection of Vortices Across Overset Interfaces[R].AIAA Paper,2005-1263,2005.
  • 5Yeshala N,Egolf T A,Vasilescu R.Application of Higher Order Spatially Accurate Schemes to Rotors in Hover[R].AIAA Paper,2006-2818,2006.
  • 6Hariharan N,Sankar L N.Unsteady overset simulation of rotor-airframe interaction[J].Journal of Aircraft,2003, 40 (4):662-674.
  • 7Wissink A,Jayaraman B,Datta A,et al.Capability Enhancements in Version 3 of the Helios High-Fide-lity Rotorcraft Simulation Code[R].AIAA Paper,2012-0713,2012.
  • 8Jameson A.Time Dependent Calculations using Multigrid,with Applications to Unsteady Flows Past Airfoils and Wings[R].AIAA Paper,91-1596,1996.
  • 9Caradonna F X,Tung C.Experimental and Analytical Studies of a Model Helicopter Rotor in Hover[R].NASA TM,81232,1981.
  • 10Meakin R L.A New Method for Establishing Inter-grid Communication Among Systems of Overset Grids[R].AIAA Paper,1991-1586,1991.

共引文献1

同被引文献15

引证文献1

二级引证文献2

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