·2,447,543篇论文数据，部分数据来源于NoteExpress
The physical solution of the initial and boundary problems of the rocket and missile impingement with complex shock structures in arbitrary bounded flow fields has been calculated in this paper.
本文对一般具有不规则边界的含复杂激波系的火箭导弹射流冲击流场初边值问题的物理解进行了计算。
youdao
应用推荐
模块上移
模块下移
不移动