摘要
本文对两种铺层的复合材料柔性梁进行了静、动特性的试验研究,重点研究了挠度、结构耦合、梁的根部安装角等对变形、固有频率的影响。得出的结论有助于直升机旋翼桨叶的设计和发展。
Experimental investigation of static and dynamic behaviors of flexible composite beams is made to study the deformation and natural frequency of beams affected by deflection,structurally coupled property and root angle.The results are useful for designing composite rotor blades under large deflection and for developing and verifing the analytical model of composite blades under large deflection.
出处
《实验力学》
CSCD
北大核心
1997年第1期59-63,共5页
Journal of Experimental Mechanics
基金
航空科学基金
关键词
大挠度
柔性梁
结构耦合
复合材料
飞机
large deflection,flexible composite beam,structurally coupled property.