机译:加速蠕变条件下用于航空涡轮叶片的热障涂层高温合金的耐损伤性
National Metallurgical Laboratory (CSIR), Jamshedpur-831 007, India;
Defence Metallurgical Research laboratory, Hyderabad-500 058, India;
Defence Metallurgical Research laboratory, Hyderabad-500 058, India;
International Advanced Research Centre for Powder Metallurgy and New Materials(ARCI), Hyderabad -500 005, India;
Defence Metallurgical Research laboratory, Hyderabad-500 058, India;
Defence Metallurgical Research laboratory, Hyderabad-500 058, India;
thermal barrier coating; substrate; creep; tensile; finite element; fractography; trans-granular; intergranular; spallation;
机译:航空涡轮机燃烧室衬里的热障涂层高温合金的抗疲劳和蠕变损伤性能
机译:航空涡轮机燃烧室衬里的热障涂层高温合金的抗疲劳和蠕变损伤性能
机译:航空涡轮机叶片用热障涂层AE 437A镍基高温合金的应力断裂行为
机译:电化学技术采用先进燃气涡轮叶片的蠕变损伤和寿命损伤和寿命预测的无损舒适
机译:各向异性复合材料中雷电引起的热消融损伤的建模及其在风力涡轮机叶片中的应用。
机译:镍基超合金汽轮机叶片温度和热应力场的热流体固体耦合分析
机译:航空发动机涡轮叶片上隔热涂层的新散裂机理
机译:双层热障涂层涡轮叶片热接触电阻的意义