Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results
计量
- 文章访问数: 134
- HTML全文浏览量: 42
- PDF下载量: 6
引用本文: | 何开锋, 王文正, 钱炜祺. 根据风洞试验结果建立有尾翼导弹数学模型[J]. 实验流体力学, 2004, 18(4): 62-66. DOI: 10.3969/j.issn.1672-9897.2004.04.014 |
Citation: | Mathematic modeling for the missile aerodynamics with tail- wing according to wind-tunnel test results[J]. Journal of Experiments in Fluid Mechanics, 2004, 18(4): 62-66. DOI: 10.3969/j.issn.1672-9897.2004.04.014 |