机译:损伤耦合弹塑性本构模型及其在涡轮叶片低周疲劳寿命预测中的应用
School of Energy and Power Engineering Beihang University Beijing 100191 China;
School of Energy and Power Engineering Beihang University Beijing 100191 China Collaborative Innovation Center of Advanced Aero-Engine Beijing 100191 China National Key Laboratory of Science and Technology on Aero-Engine Aero-mermodynamics Beijing 100191 China Beijing Key Laboratory of Aero-Engine Structure and Strength Beijing 100191 China;
School of Energy and Power Engineering Beihang University Beijing 100191 China Collaborative Innovation Center of Advanced Aero-Engine Beijing 100191 China Beijing Key Laboratory of Aero-Engine Structure and Strength Beijing 100191 China;
Army Aviation Institution Army Aviation School Beijing 100121 China;
Continuum damage mechanics; Elastic-plastic constitutive model; Low cycle fatigue; Life prediction; Turbine blade;
机译:低周疲劳寿命预测的幂指数函数模型及其应用第二部分:蠕变疲劳作用下涡轮叶片的寿命预测
机译:基于损伤力学的高低周疲劳组合寿命预测模型及其在确定叶片渗铝位置中的应用
机译:基于损伤力学的基于损伤力学的高和低循环疲劳寿命预测模型及其在确定汽轮机叶片铝化位置的应用
机译:用于燃气轮机叶片高温合金中低循环疲劳的生命预测研究
机译:高温下低周疲劳寿命的一般损伤方程。
机译:涡轮叶片寿命的高低周疲劳组合模型
机译:汽轮机叶片寿命预测的高低周疲劳组合模型
机译:美国高周疲劳数据库在风力机叶片寿命预测中的应用