A skin design method of variable camber wing trailing edge

Q3 Engineering 西北工业大学学报 Pub Date : 2023-04-01 DOI:10.1051/jnwpu/20234120329
Yonghong Zhang, Shuangquan Tang, Miao Wang, Chengmin Wang, W. Ge
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引用次数: 0

Abstract

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.
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变弧度机翼后缘蒙皮设计方法
蒙皮作为机翼的重要组成部分,其变形精度直接影响飞机在不同环境下的气动性能。基于易加工易变形的思想,提出了变弧度机翼后缘变截面厚度蒙皮的设计方法。本文首先对3~8段尾缘蒙皮的各段厚度和长度进行了优化。然后对比分析了不同皮段的变形结果。最后,通过叠皮实验验证了设计结果的正确性和方法的有效性。
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来源期刊
西北工业大学学报
西北工业大学学报 Engineering-Engineering (all)
CiteScore
1.30
自引率
0.00%
发文量
6201
审稿时长
12 weeks
期刊介绍:
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