Overset grid technology development at NASA Ames Research Center

被引:74
作者
Chan, William M. [1 ]
机构
[1] NASA, Ames Res Ctr, Moffett Field, CA 94035 USA
关键词
GENERATION; COMPUTATION; FLOW;
D O I
10.1016/j.compfluid.2008.06.009
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The idea of overset grids arose from the need to model complex multi-component systems where an optimum body-fitted grid is used for each component. One of the main motivations behind the overset grid development work at NASA originated from the requirement to perform simulations involving multiple bodies in relative motion. This article traces the development of overset grid technologies at NASA Ames Research Center, including: data format and visualization software; and algorithms and software tools for surface grid generation, volume grid generation, domain connectivity, forces and moments Calculation. and flow solution computation. Examples of the use of overset grids for NASA aerospace applications are given, and current and future work to improve overset grid technologies are summarized. Published by Elsevier Ltd.
引用
收藏
页码:496 / 503
页数:8
相关论文
共 53 条
  • [1] AHMAD JU, 2005, P 2005 ASME FLUIDS E
  • [2] [Anonymous], 2008, P AHS SPECIALISTSCON
  • [3] [Anonymous], 19941925 AIAA
  • [4] COMPUTATION OF A CONTROLLED STORE SEPARATION FROM A CAVITY
    ATWOOD, CA
    [J]. JOURNAL OF AIRCRAFT, 1995, 32 (04): : 846 - 852
  • [5] FLOWFIELD SIMULATION ABOUT THE STRATOSPHERIC OBSERVATORY FOR INFRARED ASTRONOMY
    ATWOOD, CA
    VANDALSEM, WR
    [J]. JOURNAL OF AIRCRAFT, 1993, 30 (05): : 719 - 727
  • [6] Benek J., 1985, AIAA Paper 1985-1523
  • [7] Buning P.G., 2004, AIAA Paper No. 2004-4838
  • [8] BUNING PG, 1988, 19884359 AIAA
  • [9] CHADERJIAN NM, 2006, P 4 INT C COMP FLUID
  • [10] Chan W.M., 2002, 20023191 AIAA