Structural optimization design of adaptive wing trailing edge based on multi-section mechanism

摘要：

The optimum aerodynamic configuration of the aircraft will change in order to obtain a higher lift-drag ratio for different flight conditions.Adaptive wing trailing edge (ATE) makes it possible for the wing profile to be optimal constantly.

关键词： adaptive wing trailing edge multi-section mechanism structural optimization design

作者: XINTONG SHI YU YANG

作者单位: Aircraft Strength Research Institute of China,NO.86 2nd Dianzi Road,Xian,China

会议类型: 国际会议

会议名称: The 7th International Conference on Smart Materials and Nanotechnology in Engineering (第7届智能材料与纳米技术国际会议)

会议地点: 哈尔滨

会议语种:英文

页码: 1-1

在线出版日期: 2019-09-20（万方平台首次上网日期，不代表论文的发表时间）