机译:预测层状复合材料三点弯曲损伤演化的渐进损伤模型
Dalian Univ Technol, Sch Mech Engn, Minist Educ, Key Lab Precis & Nontradit Machining Technol, Dalian 116024, Peoples R China;
Dalian Univ Technol, Sch Automot Engn, Dalian 116024, Peoples R China;
Dalian Univ Technol, Sch Mech Engn, Minist Educ, Key Lab Precis & Nontradit Machining Technol, Dalian 116024, Peoples R China;
Dalian Univ Technol, Sch Mech Engn, Minist Educ, Key Lab Precis & Nontradit Machining Technol, Dalian 116024, Peoples R China;
Shanghai Aircraft Mfg Co Ltd, Shanghai 200120, Peoples R China;
Dalian Univ Technol, Sch Mech Engn, Minist Educ, Key Lab Precis & Nontradit Machining Technol, Dalian 116024, Peoples R China;
Progressive damage model; Gradual stiffness degradation rules; Damage evolution; Delamination;
机译:纤维增强热塑性复合层压层的造型损伤对三分弯装载
机译:三点弯曲装置验证薄复合材料层合板(疲劳)损伤模型的可行性
机译:一种渐进式损伤模型,用于预测复合层压板的永久性压痕和冲击损伤
机译:三点弯曲下生物可吸收复合材料的渐进损伤分析
机译:连续损坏持续损伤的持续失效模型和层压复合材料的静态分析
机译:冲击损伤对纯弯曲薄壁组合梁性能影响的试验研究
机译:纤维增强热塑性复合层压层的造型损伤对三分弯装载
机译:层合复合三点弯曲试样的损伤状态:实验 - 分析相关性研究