Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)
Testing of Folding Wingtip for Gust Load Alleviation of Flexible High-Aspect-Ratio Wing
Journal of Aircraft ( IF 2.2 ) Pub Date : 2020-09-01 , DOI: 10.2514/1.c035732 R. C. M. Cheung 1 , D. Rezgui 1 , J. E. Cooper 1 , T. Wilson 2
Journal of Aircraft ( IF 2.2 ) Pub Date : 2020-09-01 , DOI: 10.2514/1.c035732 R. C. M. Cheung 1 , D. Rezgui 1 , J. E. Cooper 1 , T. Wilson 2
Affiliation
Folding wingtips have begun to feature on recent aircraft designs, as a solution for compliance with existing airport gate width regulations while enabling high-aspect-ratio wings for lower induced...
中文翻译：
柔性大展弦比机翼阵风载荷缓解折叠翼尖试验
折叠翼尖已开始出现在最近的飞机设计中，作为符合现有机场登机口宽度规定的解决方案，同时启用高纵横比机翼以降低诱导...
更新日期：2020-09-01
中文翻译：
柔性大展弦比机翼阵风载荷缓解折叠翼尖试验
折叠翼尖已开始出现在最近的飞机设计中，作为符合现有机场登机口宽度规定的解决方案，同时启用高纵横比机翼以降低诱导...
京公网安备 11010802027423号