| 多升力弹体气动伺服弹性发散分析 |
| |
| 引用本文： | 陈文俊.多升力弹体气动伺服弹性发散分析[J].战术导弹技术,1996(4):21-29. |
| |
| 作者姓名： | 陈文俊 |
| |
| 作者单位： | 航天工业总公司第三研究院 |
| |
| 摘 要： | 本文将无控二升力弹体气动弹性发散分析方法推广为有控多升力弹体气动伺服弹性发散分析方法。该方法毋需结构固有振型为原始数据,且数学工具简单。
|
| 关 键 词： | 气动弹性 发散 分析 |
ANALYSIS OF AEROSERVOELASTIC DIVERGENCE FOR THE MISSILE BODY WITH MULTIPLE POINT LIFT FORCES |
| |
| Chen Wenjun The Third Reseach Acadmy of CASC.ANALYSIS OF AEROSERVOELASTIC DIVERGENCE FOR THE MISSILE BODY WITH MULTIPLE POINT LIFT FORCES[J].Tactical Missile Technology,1996(4):21-29. |
| |
| Authors: | Chen Wenjun The Third Reseach Acadmy of CASC |
| |
| Affiliation: | Chen Wenjun The Third Reseach Acadmy of CASC |
| |
| Abstract: | The aeroelastic divergence analysis method of an uncontrolled rocket applied by two point aero- dynamic lifts is developed as that of a controlled missile body applied by multiple point aerodynamic lifts.In this method.no structural mode of vibration is required as primary data,and the mathematical tool is sim- ple. |
| |
| Keywords: | Aeroelasticity Divergence Analysis |
| 本文献已被 CNKI 维普 等数据库收录！ |
