Nonlinear progressive damage model for composite laminates used for low-velocity impact

• 作 者: 郭卫 薛璞 杨军
• 机 构: SchoolofAeronautics,ChengduAircraftDesignandResearchInstitute
• 出 处: 应用数学和力学：英文版
• 发表日期: 2013年9期
• 关键词: 复合材料层合板 损伤模型 低速冲击 叠层板 非线性 三维复合材料 连续介质力学 ABAQUS composite laminate progressive d
• 基金项目: Project supported by the National Natural Science Foundation of China （No. 11072202）

In order to effectively describe the progressively intralaminar and interlaminar damage for composite laminates,a three dimensional progressive damage model for composite laminates to be used for low-velocity impact is presented.Being applied to three-dim