摘要
针对翼面和桨叶等升力面结构，以单闭室薄壁梁为典型结构模型，讨论自适应复合材料薄壁梁的弯曲和扭转。
An analytical model of arbitrary cross section uniform single closed cell anisotropic beams is developed.The bending and torsion as well as displaced shape control of the adaptive composite single closed cell thin walled beam are examined.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1996年第S1期109-113,共5页
Acta Aeronautica et Astronautica Sinica
基金
航空科学基金
关键词
自适应复合材料
结构形状控制
薄壁梁
adaptive composite structure shape control thin walled beam
