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机译:基于Ni的高温合金叶片的竞争性开裂行为和微观机理,各自加速CCF衰竭
Department of Aeronautics and Astronautics Fudan University Shanghai 200433 PR China;
School of Aeronautics Science and Engineering Beihang University Beijing 100191 PR China;
China Ship Development and Design Center Wuhan 430064 PR China;
Department of Aeronautics and Astronautics Fudan University Shanghai 200433 PR China;
Department of Aeronautics and Astronautics Fudan University Shanghai 200433 PR China;
Department of Aeronautics and Astronautics Fudan University Shanghai 200433 PR China;
Turbine blade; Combined high and low cycle fatigue; Crack mode; Microstructural feature; Damage mechanism;
机译:用铝化涂层的Ni基超合金涡轮机叶片的维修损伤机理及界面开裂行为
机译:基于Ni的单晶高温合金高温疲劳裂纹生长机制的电子 - 微观分析
机译:镍基高温合金的高温疲劳和蠕变疲劳行为:损伤机理和寿命评估
机译:内外氢条件下,析出强化的镍基高温合金718与氢有关的断裂的裂纹萌生和传播方式的变化
机译:焊接沉淀淬火镍氢化Ni的超合金
机译:镍基高温合金单晶涡轮叶片根部缺陷的产生
机译:用于刀片应用的单晶Ni基超合金中的疲劳行为