期刊文献+

Enhancement and Application of Overset Grid Assembly 被引量:8

Enhancement and Application of Overset Grid Assembly
原文传递
导出
摘要 In this article, the overset grid assembly method is improved to efficiently solve several critical problems that occur when applying overset grids to the complicated geometries and moving body. First, instead of using the two-step searching (i.e. cut and paste), a single-step searching method based on the grid cell size is proposed to modify holes and optimize the grid overlapping automatically. Second, discrepancies between the wall surface representations, where the grids overlap, are handled by introducing the wall's normal directions to the hole-map and projecting the interpolated points on the recipient mesh into the donor mesh. Finally, the dynamic overset method is modified to address the complex moving body problem. At every time step, the initial hole surface of the previous time step is dynamically adjusted to accomplish hole cutting and avoid the time consuming hole-map procedure. Numerical experiments show that the enhanced overset grid assembly method obtains satisfactory results. In this article, the overset grid assembly method is improved to efficiently solve several critical problems that occur when applying overset grids to the complicated geometries and moving body. First, instead of using the two-step searching (i.e. cut and paste), a single-step searching method based on the grid cell size is proposed to modify holes and optimize the grid overlapping automatically. Second, discrepancies between the wall surface representations, where the grids overlap, are handled by introducing the wall's normal directions to the hole-map and projecting the interpolated points on the recipient mesh into the donor mesh. Finally, the dynamic overset method is modified to address the complex moving body problem. At every time step, the initial hole surface of the previous time step is dynamically adjusted to accomplish hole cutting and avoid the time consuming hole-map procedure. Numerical experiments show that the enhanced overset grid assembly method obtains satisfactory results.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2010年第6期631-638,共8页 中国航空学报(英文版)
基金 National Natural Science Foundation of China (90716010)
关键词 overset grid hole-map hole-surface optimization surface grid overset dynamic overset overset grid hole-map hole-surface optimization surface grid overset dynamic overset
  • 相关文献

参考文献1

二级参考文献13

  • 1Pearce D G, Stanley S A, Martin F W, Jr. Development of a large scale chimera grid system for the space shuttle launch vehicle[R]. AIAA-1993- 533, 1993. 被引量:1
  • 2Rogers S E, Cao H V, Su T Y. Grid generation for complex high-lift configurations[R]. AIAA-1998-3011, 1998. 被引量:1
  • 3Murman S M, Rizk Y M, Schiff L B. Coupled numerical simulation of the external and engine inlet flows for the F- 18 atlarge incidence[J]. Aircraft Design, 2000, 3(2): 65- 77. 被引量:1
  • 4Benek J A, Buning P G, Steger J L. A 3-D chimera grid embedding technique[R]. A1AA-1985 1523, 1985. 被引量:1
  • 5Meaking R L. A new method for establishing intergrid communication among systems of overset grids [R]. AIAA-1991 -1586, 1991. 被引量:1
  • 6Nakahashi K, Togashi F, Sharov D. Intergrid-boundary definition method for overset unstructured grid approach [J]. AIAA Journal, 2000, 38(11): 2077-2084. 被引量:1
  • 7Wey T C. Development of a mesh interface generator for overlapped structured grids[R]. AIAA 1994- 1924, 1994. 被引量:1
  • 8Cho K W, Kwon J H. Development of a fully systemized chimera methodology for steady/unsteady prohlems[J]. Journal of Aircraft, 1999, 36(6): 973- 980. 被引量:1
  • 9Noack R W. Resolution appropriate overset grid assembly for structured and unstructured grids [R]. AIAA 2003 4123, 2003. 被引量:1
  • 10Rogers S E, Suhs N E, Suhs W E. Pegasus 5: an automa ted preprocessor for overset grid computational fluid dynamics[J]. AIAA Journal, 2003, 41 (6) : 1037-1045. 被引量:1

共引文献13

同被引文献28

  • 1黄雪樵.克服欧拉方程奇异性的双欧法[J].飞行力学,1994,12(4):28-37. 被引量:30
  • 2李亭鹤,阎超,李跃军.重叠网格技术中割补法的研究与改进[J].北京航空航天大学学报,2005,31(4):402-406. 被引量:6
  • 3李跃军,阎超.飞行器姿态角解算的全角度双欧法[J].北京航空航天大学学报,2007,33(5):505-508. 被引量:19
  • 4范晶晶.复杂重叠网格方法研究及多体运动的非定常流动模拟[D].北京:北京航空航天大学航空科学与工程学院,2010. 被引量:4
  • 5Liever P, Habchi S. Separation analysis of launch vehicle crewescape systems [ R ] . AIAA Paper, 2004 - 4726,2004. 被引量:1
  • 6Kim J, Park S, Yu Y. Euler and navier ~ stokes simulations ofhelicopter rotor blade in forward flight using an overlapped gridsolver[ R] . AIAA Paper 2009 -4268,2009. 被引量:1
  • 7Steger J, Dougherty F, Benek J. A chimera grid scheme[C].ASME Mini-Symposium on Advances in Grid Generation, 1982. 被引量:1
  • 8Suhs N, Rogere S, Dietz W. Pegasus 5: an automated pre-processor for overset-grid CFD[ R] . AIAA Paper 2002 - 3186,2002. 被引量:1
  • 9Noack H. Resolution appropriate overset grid assembly forstructured and unstructured grids[C]. 16lh AIAA ComputationalFluid Dynamic Conference, Paper 2003 -4123 , 2003. 被引量:1
  • 10Belk D, Maple R. Automated assembly of structured grids formoving body problems [ C ]. Proceedings of 12th AIAAComputational Fluid Dynamics Conference, AIAA Paper 95 -1680-CP,1995. 被引量:1

引证文献8

二级引证文献25

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