| 回归分析方法在气动弹性研究中的应用 |
| |
| 引用本文： | 李增文,曾江红. 回归分析方法在气动弹性研究中的应用[J]. 战术导弹技术, 2004, 0(4): M026-28 |
| |
| 作者姓名： | 李增文 曾江红 |
| |
| 作者单位： | 中国航天科工集团公司第三研究院,北京100074 |
| |
| 摘 要： | 介绍了回归分析方法在某飞行器尾翼颤振研究过程中的应用.通过程序自动分析, 使用检验方法, 逐步获得与颤振裕度相关的频率因子, 得到仅含有显著相关频率因子的最优回归方程.分析表明, 此方法得到的颤振裕度回归方程满足工程设计需要.
|
| 关 键 词： | 颤振速度 回归分析 颤振裕度 |
| 文章编号： | 1009-1300(2004)04-0026-03 |
| 修稿时间： | 2004-03-24 |
Application of Regress Analysis Method to Aeroelasticity Research |
| |
| Li Zengwen,Zeng Jianghong. Application of Regress Analysis Method to Aeroelasticity Research[J]. Tactical Missile Technology, 2004, 0(4): M026-28 |
| |
| Authors: | Li Zengwen Zeng Jianghong |
| |
| Abstract: | The regress analysis method is used in tail flutter computation. Through the automatic analysis, the frequency factors are gotten which are related to flutter margin, the optimizing equation is also obtained which is expressed by the remarked frequency factor. The analysis results show that the flutter margin regress equation meets the needs of engineering. |
| |
| Keywords: | flutter velocity regress analysis flutter margin |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
