机译:基于非线性连续体损伤力学和临界平面方法的多轴疲劳寿命预测
State Key Laboratory of Mechanics and Control of Mechanical Structures Nanjing University of Aeronautics and Astronautics;
State Key Laboratory of Mechanics and Control of Mechanical Structures Nanjing University of Aeronautics and Astronautics;
State Key Laboratory of Mechanics and Control of Mechanical Structures Nanjing University of Aeronautics and Astronautics;
State Key Laboratory of Mechanics and Control of Mechanical Structures Nanjing University of Aeronautics and Astronautics;
critical plane approach; damage mechanics; GH4169; life prediction; multiaxial fatigue;
机译:基于非线性连续体损伤力学和临界平面方法的多轴疲劳寿命预测
机译:基于临界面法的中碳钢多轴疲劳损伤参数及寿命预测
机译:连续损伤力学方法预测橡胶状材料在多轴载荷下的疲劳寿命:两嵌段载荷和R比的影响
机译:连续损伤力学方法的多轴疲劳寿命预测橡胶状材料
机译:均质和非均质材料多轴疲劳寿命预测的临界平面能量模型。
机译:涡轮叶片多轴疲劳寿命预测的新的能量临界平面损伤参数
机译:基于临界面连续损伤力学和遗传算法的新型混合多轴疲劳寿命模型
机译:CaREs /蠕变的确定性和概率蠕变和蠕变断裂增强:用连续损伤力学和有限元法预测陶瓷结构的多轴蠕变寿命