摘要
文中采用了并行计算来研究单元数对计算速度的影响;分析了不同的边界条件对计算气动力特性的影响;并探讨了计算流场所需的软硬件支持。为利用商业流体软件来计算火箭弹的气动力特性提供了有效的总结和指导。
The influence factor of computational speed about elements was researched in this paper, by using the method of parallel compute, and of aerodynamic property was analyzed in the condition of different boundary condition. In addition, configuration of software and hardware on analyzing fluid field was researched. Summarization and instruction were provided effectively for people who compute aerodynamic property of rocket shell hy using trade fluent soft.
出处
《弹箭与制导学报》
CSCD
北大核心
2005年第3期78-80,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
并行计算
流场
气动力特性
火箭弹
parallel compute
fluid field
aerodynamic property
rocket
