机译:非比例载荷下的多轴疲劳损伤参数研究
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;
Department of Civil and Structural Engineering, The University of Sheffield, Sheffield SI 3JD, UK;
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;
direct damage parameters; equivalent damage parameters; multiaxial fatigue; nonproportional additional hardening;
机译:比例和非比例载荷下用于多轴疲劳寿命预测的广义疲劳损伤参数
机译:非比例载荷下多轴疲劳损伤参数和寿命预测方法的开发
机译:基于瞬时疲劳损伤跟踪的复杂几何形状和随机非比例载荷条件下的零件新的多轴HCF准则
机译:非比例多轴荷载下MOD.9CR-1MO钢的低循环疲劳损坏
机译:复杂非比例载荷条件下的多轴疲劳分析
机译:寿命相关材料参数在多轴非零均值载荷下疲劳寿命预测中的应用
机译:非比例荷载下多轴疲劳损伤参数的研究
机译:多轴变形测试:非比例加载和高温