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机译:低速冲击坑Al-Si-Mg铝合金疲劳试验及损伤模型开发
School of Aeronautic Science and Engineering Beihang University Beijing 100191 China;
School of Aeronautic Science and Engineering Beihang University Beijing 100191 China;
Hunan Aviation Powerplant Research Institutee Aero Engine (Group) Corporation of China Zhuzhou 412002 China;
School of Aeronautic Science and Engineering Beihang University Beijing 100191 China;
School of Aeronautic Science and Engineering Beihang University Beijing 100191 China Shen Zhen Institute of Beihang University Shenzhen 518000 China;
Aluminum alloy; Impact pit; Continuum damage mechanics; Fatigue life; Damage evolution model;
机译:模拟铸造Al-Si-Mg铝合金中应力状态相关的损伤演化
机译:基于连续损伤力学的7050-T7451铝合金冲击坑疲劳寿命预测方法
机译:旋转弯曲疲劳试验中两个人工点孔的接近度和尺寸对铝合金AlSI 6061-T6疲劳强度的影响
机译:两种人工点蚀孔的接近度和尺寸对旋转弯曲疲劳试验下铝合金6061-T6疲劳强度的影响
机译:使用粘弹性连续损伤模型开发简化的疲劳测试和分析程序,并将其应用于WesTrack混合物。
机译:基于DIC的2024-T4预腐蚀铝合金疲劳损伤演变的研究
机译:6061-T6铝合金的旋转弯曲疲劳测试,接近弹性极限并带有人工点蚀孔
机译:利用实用无损检测技术检测金属和合金疲劳损伤的测试装置的研制