دورية أكاديمية
A skin design method of variable camber wing trailing edge
| العنوان: | A skin design method of variable camber wing trailing edge |
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| المؤلفون: | ZHANG Yonghong, TANG Shuangquan, WANG Miao, WANG Chengmin, GE Wenjie |
| المصدر: | Xibei Gongye Daxue Xuebao, Vol 41, Iss 2, Pp 329-337 (2023) |
| بيانات النشر: | EDP Sciences, 2023. |
| سنة النشر: | 2023 |
| المجموعة: | LCC:Motor vehicles. Aeronautics. Astronautics |
| مصطلحات موضوعية: | 变弯度机翼后缘, 变截面厚度蒙皮, 上、下缘蒙皮曲率, Motor vehicles. Aeronautics. Astronautics, TL1-4050 |
| الوصف: | 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. |
| نوع الوثيقة: | article |
| وصف الملف: | electronic resource |
| اللغة: | Chinese |
| تدمد: | 1000-2758 2609-7125 20234120 |
| العلاقة: | https://www.jnwpu.org/articles/jnwpu/full_html/2023/02/jnwpu2023412p329/jnwpu2023412p329.htmlTest; https://doaj.org/toc/1000-2758Test; https://doaj.org/toc/2609-7125Test |
| DOI: | 10.1051/jnwpu/20234120329 |
| الوصول الحر: | https://doaj.org/article/eaac7a17bb754f22ad67f9f5386e6a21Test |
| رقم الانضمام: | edsdoj.7a17bb754f22ad67f9f5386e6a21 |
| قاعدة البيانات: | Directory of Open Access Journals |
Full Text Finder | تدمد: | 10002758 26097125 20234120 |
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| DOI: | 10.1051/jnwpu/20234120329 |