A skin design method of variable camber wing trailing edge

被引：0
|
作者：
Zhang Y. [1 ]
Tang S. [1 ]
Wang M. [1 ]
Wang C. [1 ]
Ge W. [1 ]
机构：
[1] School of Mechanical Engineering, Northwestern Polytechnical University, Xi′an
来源：
Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University | 2023年 / 41卷 / 02期
关键词：
lower edge skin curvature; upper; variable camber wing trailing edge; variable section thickness skin;
D O I：
10.1051/jnwpu/20234120329
中图分类号：
学科分类号：
摘要：
As an important part of the wing, the skin deformation accuracy directly affect the aerodynamic performance of the aircraft in different environments. Based on the idea of easy processing and easy deformation, a method for designing variable section thickness skin for trailing edge of variable camber wings is proposed. In this paper, firstly, the thickness and length of each segment of 3 ~ 8 segments of trailing edge skin are optimized. Then the deformation results of different segments of skin are compared and analyzed. Finally, the correctness of the design results and the effectiveness of the method are verified by using stacked skin experiment. ©2023 Journal of Northwestern Polytechnical University.
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页码：329 / 337
页数：8
相关论文
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