机译:相似寿命载荷在多轴两步阶跃谱下的累积疲劳损伤规律研究
Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
2024-T4 aluminium alloy; accumulative damage rule; damage evolution; multiaxial fatigue; two-stage step spectrum;
机译:考虑载荷振幅和载荷路径变化的多轴阶梯谱累积疲劳损伤模型
机译:2024-T4铝合金在多轴块载荷谱下累积损伤规律的比较研究
机译:基于能量的损伤描述,以评估经过各种多轴加载光谱的钢样品的疲劳寿命
机译:非营销多轴荷载下估算低循环疲劳寿命的损伤模型
机译:复杂多轴载荷下航空航天材料疲劳损伤的表征
机译:CFRP加固钢筋混凝土梁的疲劳寿命预测:基于累积损伤模型的研究
机译:振动负荷下横盾隧道结构的动态特性和疲劳累积损伤