| 基于ADAMS/Aircraft的舰载机逃逸性能分析 |
| |
| 引用本文： | 史卫民,韩维,李辉青.基于ADAMS/Aircraft的舰载机逃逸性能分析[J].海军航空工程学院学报,2010,25(5):481-484. |
| |
| 作者姓名： | 史卫民 韩维 李辉青 |
| |
| 作者单位： | 海军装备部;海军航空工程学院七系;海军航空工程学院研究生管理大队; |
| |
| 摘 要： | 文章基于MSC ADAMS/Aircraft平台,建立了目标舰载机得起落架、轮胎、机身及全机虚拟样机模型,并进行飞机逃逸仿真分析,结果表明目标舰载机具有较好的逃逸性能。
|
| 关 键 词： | ADAMS/Aircraft 逃逸 虚拟样机 |
The Carrier-Based Aircraft Bolter Analysis Based on ADAMS/Aircraft |
| |
| SHI Wei-min,HAN Wei and LI Hui-qing.The Carrier-Based Aircraft Bolter Analysis Based on ADAMS/Aircraft[J].Journal of Naval Aeronautical Engineering Institute,2010,25(5):481-484. |
| |
| Authors: | SHI Wei-min HAN Wei and LI Hui-qing |
| |
| Institution: | 1.Naval Equipment Department,Beijing 100071,China; 2.Naval Aeronautical and Astronautical University a. №7 Department;b. Graduate Students’ Brigade,Yantai Shandong 264001,China) |
| |
| Abstract: | Based on the software ADAMS/Aircraft, the virtual prototype model of the gear, the tire, the airframe and the full aircraft were built in this paper, and the bolter process was simulated. The results show that the aircraft possesses excellent bolter capability, and the ADAMS/Aircraft provides an effective method to the dynamical analysis. |
| |
| Keywords: | ADAMS/Aircraft bolter virtual prototype |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《海军航空工程学院学报》浏览原始摘要信息 |
| 点击此处可从《海军航空工程学院学报》下载免费的PDF全文 |
