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;
Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle,Nanjing University of Aeronautics and Astronautics,Nanjing,210016,China;
multiaxial fatigue; fatigue damage rule; nonproportional loading; variable amplitude loading;
机译:顺序双轴加载下Ly12Cz铝合金疲劳损伤规律
机译:具有广泛疲劳损伤的加硬LY12CZ铝合金板的残余强度
机译:具有广泛疲劳损伤的加硬LY12CZ铝合金板的残余强度
机译:顺序双轴加载下Ly12Cz铝合金疲劳损伤规律
机译:1045钢和7075铝合金的双轴疲劳机理和寿命预测,包括各向异性和缺口效应。
机译:S-N曲线平均应力校正模型在选定铝合金随机扭转负荷的疲劳寿命估计方面的应用
机译:具有广泛疲劳损伤的加硬LY12CZ铝合金板的残余强度
机译:疲劳中的应力相互作用和累积损伤规则II.7075铝合金