| 不同柔度的柔性翼气动特性实验研究 |
| |
| 引用本文： | 徐顶国.不同柔度的柔性翼气动特性实验研究[J].航空动力学报,2011,26(1). |
| |
| 作者姓名： | 徐顶国 |
| |
| 作者单位： | 西北工业大学 |
| |
| 基金项目： | 国家自然基金项目（2008YL0100020010002） |
| |
| 摘 要： | 为了研究不同柔度的柔性翼气动特性和抗风性性能，制作了九种不同柔段的柔性翼，利用西北工业大学微型飞行器专用风洞对其进行初步的风洞试验，在实验中进行了不同风速，不同迎角对柔段的气动特性研究。通过试验优选出气动特性较好的柔段，为柔性翼微型飞行器的总体设计和气动特性提供参考。
|
| 关 键 词： | 微型飞行器 柔性翼 柔度 风洞试验 |
Investigations on aerodynamic characteristics test of different flexibility of the flexible wing |
| |
| dingguo-xu.Investigations on aerodynamic characteristics test of different flexibility of the flexible wing[J].Journal of Aerospace Power,2011,26(1). |
| |
| Authors: | dingguo-xu |
| |
| Institution: | NorthwesternPolytechnical University |
| |
| Abstract: | In order to study aerodynamic characteristics and wind-resistance performance of different flexibility of the flexible wing, we have produced nine different flexibiltty of the flexible wing micro air vehicles, the wind tunnel test is performed in special micro air vehicle wind tunnel of NPU (Northwestern Polytechnical University). The influence of wind velocity, angle of attack on aerodynamic characteristics is investigated and the aerodynamic characteristics of a good flexibility ofthe flexible wing micro air vehicle was Optimized. The result of experiment can guide us in conceptual design and aerodynamic design of flexible-wing MAV. |
| |
| Keywords: | Micro Air Vehicle flexible wing flexibility wind tunnel test |
|
| 点击此处可从《航空动力学报》浏览原始摘要信息 |
| 点击此处可从《航空动力学报》下载免费的PDF全文 |
