| 轻型无人机复合材料机翼设计分析与验证 |
| |
| 引用本文： | 张军红,李国民.轻型无人机复合材料机翼设计分析与验证[J].西安航空技术高等专科学校学报,2013(3):33-36. |
| |
| 作者姓名： | 张军红 李国民 |
| |
| 作者单位： | 中国电子科技集团公司第三十八研究所 |
| |
| 摘 要： | 基于轻型无人机复合材料的机翼,在选定机翼构件布局、材料和构型,建立机翼结构有限元模型的基础上,计算分析了机翼的静强度、应力分布,并对其进行试验验证。该方法对中小型复合材料无人机结构设计和静强度试验具有一定的参考价值。
|
| 关 键 词： | 轻型无人机 复合材料机翼 静强度 力学性能 |
Light UAV Composite Wing Design,Analysis and Verification |
| |
| ZHANG Jun-hong,Li Guo-min.Light UAV Composite Wing Design,Analysis and Verification[J].Journal of Xi'an Aerotechnical College,2013(3):33-36. |
| |
| Authors: | ZHANG Jun-hong Li Guo-min |
| |
| Institution: | (No.38Research Institute of CETC,Hefei 230088,China) |
| |
| Abstract: | The wing configuration of light UAV （unmanned aerial vehicles） is established, the material of each wing structure unit is selected and its FEM model is created. On the basis, the paper carries out analysis on static strength and stress distribution of wings, and the results are consistent with experimental data. This method has the given referential value for the structural design and static strength test of small and medium-sized composite UAV. |
| |
| Keywords: | UAV composite material wing static strength mechanical property |
| 本文献已被 CNKI 维普 等数据库收录！ |
|
