有限元法
结构工程
材料科学
航空航天
失效模式及影响分析
钢筋
螺栓连接
复合材料层合板
残余应力
计算机模拟
模式(计算机接口)
热的
压力(语言学)
残余物
复合数
承载力
方位(导航)
集合(抽象数据类型)
材料性能
复合材料
承重
耐久性
残余强度
工程类
设计工具
灵敏度(控制系统)
机械工程
标识
DOI:10.1016/j.compstruct.2026.120152
摘要
Local metal hybridization with steel plies offers an effective route to improve the bolt-bearing performance of CFRP structures. This study develops and validates a finite element framework for hybrid CFRP–steel bolted joints, with emphasis on the role of thermal residual stresses and delamination. The modeling approach is validated against a comprehensive set of bolt-bearing tests at 23 °C and -55 °C, demonstrating accurate reproduction of load-displacement curves up to 4% elongation in monolithic CFRP and up to 10% in hybrid laminates. Analysis of reinforcement mechanisms shows that steel plies relieve stress in the composite, delay damage initiation, and confine damage within composite stacks, thereby increasing the load bearing capacity of the joint. Geometry studies further reveal the correct prediction of failure mode transitions with decreasing specimen width, indicating a critical width-to-diameter ratio of 4-5 for QI-FML joints. The validated framework thus provides predictive capability and mechanistic insight for design and virtual testing of aerospace joints.
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