摘要
利用分区计算技术 ,从 Euler方程出发 ,应用三维隐式有限体积 TVD格式 ,数值模拟了飞机悬停状态时某机载导弹机弹相容流场 ,计算结果详细给出了燃气射流及其对翼壁压力的非定常发展过程 。
Based on zonal approach, the compatible flowfield of plane hanging in the air and missile jet are numerically simulated. The three dimensional Euler equations and implicit finite volume TVD scheme are applied. The calculation shows the unsteady development of the jet field and the pressure on the plane detailedly, and the result can provide theoritical foundation for the study of compatibility of plane and missile.
出处
《弹道学报》
EI
CSCD
北大核心
2001年第1期10-15,共6页
Journal of Ballistics
