基于交叉簧片式铰链的变弯度机翼机构设计
徐钧恒,杨晓钧,李兵
Design of wing mechanism with variable camber based on cross-spring flexural pivots
Jun-heng XU,Xiao-jun YANG,Bing LI
图 15
变弯度机翼实验平台
Fig.15
Parameter definition of flexible trailing edge sub element