空气动力学学报2013，Vol.31Issue(3)：288-293,6.
带控制律导弹投放数值模拟
Missile separation simulation with control laws
周乃春 1李彬 1郑鸣 1邓有奇1
作者信息
- 1. 中国空气动力研究与发展中心计算所,四川绵阳 621000
- 折叠
摘要
Abstract
Using an overset unstructured grid,three dimensional URANS equations are applied to simulate the missile separation with control laws.The walls criterion is used in the automatic hole-cutting procedure.Arithmetic average method is used to get the value during the overset grids.Comparison computing of the trajectories of a wing/pylon/finned-store configuration with three different control laws is carried out with this method,and a complex separation problem is solved.关键词
URANS方程/非结构重叠网格/舵面控制律Key words
URANS equation/ overset unstructured grid/ control law分类
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周乃春,李彬,郑鸣,邓有奇..带控制律导弹投放数值模拟[J].空气动力学学报,2013,31(3):288-293,6.
