|
|||||
|
|
| 机翼颤振模型的结构动力学设计 | |
| 引用本文： | 成志清 陈怀海. 机翼颤振模型的结构动力学设计[J]. 振动工程学报, 1995, 8(2): 184-189 |
| 作者姓名： | 成志清 陈怀海 |
| 作者单位： | 南京航空航天大学振动工程研究所 |
| 摘 要： | 介绍了围绕某型飞机机翼颤振模型的结构动力学设计所开展的研究工作，内容包括设计目标与设计参数的确定、设计模型与设计变量的选取、设计方法与优化方法、主体结构与边界条件设计等。试验结果表明，设计出的颤振模型满足预定的振动特性要求。 |
| 关 键 词： | 机翼 颤振 结构动力学 模态试验 风洞试验 |
Dynamic Design of a Flutter Model of Airfoil |
|
| Cheng Zhiqing Chen Huaihai. Dynamic Design of a Flutter Model of Airfoil[J]. Journal of Vibration Engineering, 1995, 8(2): 184-189 | |
| Authors: | Cheng Zhiqing Chen Huaihai |
| Abstract: | This paper discribes the investigation on dynamic design of a nutter model.The contents include the determination of design object and design parameters,the selection of design model and design variables,the design and optimization methods las well as the design of primary structure and boundary conditions.Experiment results show that the flutter model designed can meet the requirements predetermined. |
| Keywords: | wing flutter structural dynamic design flutter model of airfoil modal tests wind tunnel tests |
| 本文献已被 CNKI 维普 等数据库收录！ | |