摘要
基于Wilson非协调元技术和Reddy逐层理论(LWM),提出了非协调逐层法(ILWM),用于分析层合板壳结构的弯曲变形问题。推导了非协调逐层法的控制方程,并通过编写计算程序,进行算例分析,研究该方法的有效性。研究结果表明,对于弯曲问题,非协调逐层法的收敛速度和计算精度相比Reddy逐层理论都有很大的提高。
Based on Wilson incompatible element technique and Reddy 's layerwise theory( LWM),an incompatible layerwise method( ILWM) is presented to deal with the bending problems of laminated shells in this study. Derivation of the equilibrium equations of the ILWM is performed. Several examples are studied to validate the capabilities of proposed method.The numerical results indicate that The ILWM achieves better convergence rate and computational accuracy compared with LWM for bending models.
作者
张峰
余义良
郑亦媚
ZHANG Feng;YU YiLiang;ZHENG YiMei(College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, Chin)
出处
《机械强度》
CAS
CSCD
北大核心
2018年第3期660-665,共6页
Journal of Mechanical Strength
基金
中国民航大学中央高校基础科研项目(3122016D014)资助