摘要
In order to calculate the aerodynamic heating process of the missile head, the environmental temperature and pressure are obtained by the ballistic trajectory table and the flight Mach number are calculated. The method of fluidsolid coupled was used to compute the inner and outer field of the missile. The temperature of the missile surface and head was obtained. The result shows the fluid-solid coupled method is suitable for the aerodynamic heating calculation. The inflexion of the missile should be considered respectively at the subsonic and the supersonic flight in the design of the missile.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010 |
| 页 | 184-186 |
| 页数 | 3 |
| DOI | |
| 出版状态 | 已出版 - 2010 |
| 活动 | 5th International Conference on Frontier of Computer Science and Technology, FCST 2010 - Changchun, 中国 期限: 18 8月 2010 → 22 8月 2010 |
出版系列
| 姓名 | Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010 |
|---|
会议
| 会议 | 5th International Conference on Frontier of Computer Science and Technology, FCST 2010 |
|---|---|
| 国家/地区 | 中国 |
| 市 | Changchun |
| 时期 | 18/08/10 → 22/08/10 |
指纹
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Liu, B., Ma, Y., Jiang, Y., Wang, W., Li, Y., & Shao, L. (2010). Numerical simulation on aerodynamic heating process and research on the missile head structure. 在 Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010 (页码 184-186). 文章 5575513 (Proceedings - 5th International Conference on Frontier of Computer Science and Technology, FCST 2010). https://doi.org/10.1109/FCST.2010.47