| 高超音速飞行器气动特性工程计算 |
| |
| 引用本文： | 程养民.高超音速飞行器气动特性工程计算[J].固体火箭技术,2000,23(2):1-6. |
| |
| 作者姓名： | 程养民 |
| |
| 作者单位： | 中国航天科技集团公司四院四十一所,西安,710025 |
| |
| 摘 要： | 计算了某高超音速火箭的气动特性 ,并用风洞试验数据进行比较 ,验证了计算方法是可靠的。在此基础上 ,用该方法计算了高超音速导弹各种常见外形的气动特性 ,形成数据库 ,便于今后在工程上应用
|
| 关 键 词： | 导弹 高超音速 气动特性 风洞试验 数据库 |
Engineering Calculation of Aerodynamic Characteristics of Hypersonic Vehicles |
| |
| CHENG Yang-min.Engineering Calculation of Aerodynamic Characteristics of Hypersonic Vehicles[J].Journal of Solid Rocket Technology,2000,23(2):1-6. |
| |
| Authors: | CHENG Yang-min |
| |
| Abstract: | Aerodynamic characteristics of some hypersonic rockets are calculated and the results are compared with that of wind tunnel test to verify the reliability of the calculation method.The aerodynamic characteristics of some kinds of hypersonic missiles with common configuration are calculated using this method and a data base is set up based on the calculation for engineering application. |
| |
| Keywords: | guided missile hypersonic speed aerodynamic characteristic wind tunnel test data base |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
