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| 弹翼剖面弯曲刚度的确定方法 | |
| 引用本文： | 陈文俊. 弹翼剖面弯曲刚度的确定方法[J]. 系统工程与电子技术, 1996, 0(8) |
| 作者姓名： | 陈文俊 |
| 作者单位： | 航天工业总公司三院三部 |
| 摘 要： | 本文基于梁的弯曲理论和挠度测量数据提出了两个计算弹翼剖面弯曲刚度的公式，分析了影响公式精度的有关因素。说明了公式的适用范围、用户注意事项和操作程序，最后提出了扩大公式应用范围的一个设想。 |
| 关 键 词： | 飞行器，弹翼，弯曲强度，结构分析 |
A Method of Determining Fiexural Stiffnesses of Wing Sections |
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| Chen Wenjun. A Method of Determining Fiexural Stiffnesses of Wing Sections[J]. System Engineering and Electronics, 1996, 0(8) | |
| Authors: | Chen Wenjun |
| Affiliation: | The Third Research Academy of CASC. Beijing 100074 |
| Abstract: | Based on beam fiexural theory and measured deflection data. this paper presents two formulas of calculating flexural stiffnesses of wing sections. analyzes some factors related to the accuracy of these formulas. discusses their applicable scope. makes clear the points of attention and the operating procedure. Finally it Presents an idea of extending the applicable scope of these formulas. |
| Keywords: | Wing Flexural stiffnesses of Sections. |
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