复合材料弯扭耦合机翼结构分析模型研究进展

摘要

本文将复合材料弯扭耦合机翼结构分析模型分为二维板模型和薄壁梁模型，对复合材料弯扭耦合机翼结构分析模型进行了系统回顾和综述，对比分析了其优缺点，并总结了相关研究方法和成果。%In this paper, several analysis models, which have been proposed to conduct the bend-twist coupling design of composite wing structures, were reviewed and evaluated. All those models were divided into two parts:two-dimensional plate models and thin-walled beam models. And their advantages and disadvantages were objectively listed and compared. Finally, some achievements of the corresponding study methods were summarized.