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
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China|Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China|Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China|Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;
AVIC CAPDI Integrat Equipment Co Ltd, Beijing 100120, Peoples R China;
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China|Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China|Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China|Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;
Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;
CCF test; Life prediction model; Damage mechanics; Nonlinear interaction; Aluminizing treatment;
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:基于阈值损伤的基于高低循环疲劳下涡轮机叶片的疲劳寿命预测
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:预测复合循环疲劳的燃气轮机叶片寿命的实验方法和CAILLETAUD材料模型的发展
机译:基于能量的高,低和联合循环疲劳寿命预测方法的多尺度分析和扩展。
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