考虑后屈曲的复合材料加筋壁板承载能力分析

Load Carrying Capacity Analysis of Stiffened Composite Panel Considering Post- buckling

复合材料加筋结构的承载能力预估是飞机设计中的重要内容,其关键问题就是考虑材料失效的后屈曲分析。针对复合材料加筋壁板承受压缩载荷的后屈曲承载能力预估问题,考虑层内损伤、层间分层以及刚度退化,基于内聚力单元与Hashin损伤准则,建立了一种简洁的渐进损伤分析方法,编制了相应的ABAQUS UMAT子程序,并利用复合材料加筋结构破坏试验进行了验证。验证结果表明,预估的承载能力、破坏模式和结构应力状态与物理试验结果符合得很好,承载能力误差在10%以内,证明了方法的准确性和工程实用性。

The load carrying capacity prediction of stiffened composite structure is an important part of aircraft designing,and the key problem is post-buckling analysis taken material failure into account.A concise progressive damage analysis methodology considering intralaminar failure,delamination and stiffness degradation was established based on cohesive elements and Hashin damage criteria subjected to the post-buckling analysis beared compressive loading,and UMAT subroutines of ABAQUS were developed.The comparison indicates that the load carrying capacity,failure mode and strain analysis results of this paper agree well with test results,and the relative error is less than 10% which proves the effectiveness of the present methodology.