期刊文献+

基于二重网格的动网格松弛法改进 被引量:2

An improvement on the dynamic mesh method of sphere relaxation using double grids
下载PDF
导出
摘要 相比传统的弹簧法等方法,基于球松弛算法的动网格松弛法在复杂边界大变形条件下可以得到质量更高的边界网格以及更大的极限变形量,但该方法在时间效率上还有提升的空间。引入二重网格,采用动网格松弛法进行稀疏网格的网格变形,将边界位移传递到整个网格计算域;再利用二重网格映射,将稀疏网格位移映射到原有计算网格的节点上。算例表明,改进后的动网格松弛法在极限变形量和变形后网格质量基本保持不变的情况下,能够有效地提高网格变形的计算效率。此外还研究了二重网格的粗细网格节点数之比(粗网格为稀疏网格,细网格为原计算网格)对网格变形的影响,算例表明最佳计算效率出现在粗细网格节点数之比为0.5左右时。 The dynamic mesh method based on the sphere relaxation algorithm generates boundary meshes with higher quality and achieves larger deformation than the traditional spring method even for large boundary deformations.However,the time efficiency of this method still has room for improvement.In this work,we present a double-grid strategy which introduces a coarse mesh besides the computational mesh(fine mesh).The sphere relaxation algorithm is applied to deform the coarse mesh and transfer the boundary displacement to the entire region.Then,the double-grid mapping is carried out to map the displacements of the coarse mesh into the computational mesh.Numerical examples show that the improved method effectively increases the mesh deformation efficiency while the deformation ability and mesh quality remain.We also study the effects of the node number ratio(coarse mesh/fine mesh)on the mesh deformation.Numerical examples indicate that the optimal node number ratio is about 0.5 for the highest efficiency.
作者 廖佳文 张力天 周璇 李水乡 LIAO Jia-wen;ZHANG Li-tian;ZHOU Xuan;LI Shui-xiang(College of Engineering,Peking University,Beijing 100871,China;Institute of Applied Physics and Computational Mathematics,Beijing,100094,China)
出处 《计算力学学报》 CAS CSCD 北大核心 2022年第1期37-41,共5页 Chinese Journal of Computational Mechanics
基金 国家自然科学基金(U1630112) 科学挑战专题(JCKY2016212A502)资助项目.
关键词 二重网格 动网格 网格变形 球松弛 非结构网格 double grids dynamic mesh mesh deformation sphere relaxation unstructured grids
  • 相关文献

参考文献5

二级参考文献131

  • 1张军,谭俊杰,任登凤.HLLC方法在三维非结构网格上的应用[J].南京航空航天大学学报,2004,36(5):649-652. 被引量:1
  • 2黄冬梅,童水光,陈德华.外挂物投放问题的二维非结构动态网格技术研究[J].空气动力学学报,2006,24(1):73-79. 被引量:2
  • 3张军,谭俊杰,任登凤.副油箱从机翼分离流场的数值模拟[J].自然科学进展,2006,16(8):1033-1037. 被引量:7
  • 4PERKINS D A, REED J I., HAVENS J E. Morphing wing structures for loitering air vehicles [R]. AIAA 2004-1888.
  • 5RAMRKAHYANI D S, LESIENTURE G A. Aircraft structural morphing using tendon actuated compliant cellular trusses[R]. AIAA 2004-1728.
  • 6SECANELL M, SULEMAN A, GAMBOA P. Design of a morphing airfoil for a light unmanned aerial vehicle using high-fidelity aerodynamic shape optimization[R]. AIAA 2005-1891.
  • 7LIU H, WASSERSUG R J, KAWACHI K A. The three- dimensional hydrodynamics of tadpole locomotion [J]. J. Exp. Biol., 1997, 200: 2807-2819.
  • 8WU J W, SUN M. Unsteady aerodynamics forces of a flapping wing[J]. J. Exp. Biol., 2004(207): 1413- 1427.
  • 9NAKAHASHI K, TOGASHI F. An intergrid-boundary definition method for overset unstructured grid approach[R]. AIAA-99 3304.
  • 10LOHNER R, SHAROY D, LUO H, et al. Overlapping unstructured grids[R]. AIAA-01-0439.

共引文献51

同被引文献7

引证文献2

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