机译:预腐蚀对7050-T7651铝合金损伤发展和裂纹扩展的影响
Sino-European Institute of Aviation Engineering, Civil Aviation University of China, China,Mechanical Engineering, College of Engineering and Informatics, NUI Galway, Ireland;
Sino-European Institute of Aviation Engineering, Civil Aviation University of China, China;
Department of Materials Engineering, KU Leuven, Belgium;
Sino-European Institute of Aviation Engineering, Civil Aviation University of China, China;
Mechanical Engineering, College of Engineering and Informatics, NUI Galway, Ireland;
aluminum alloy; crack propagation; damage evolution; digital image correlation; localized corrosion;
机译:铝合金7075-T6腐蚀前疲劳寿命的等效裂纹尺寸模型
机译:Al-Mg-Si基锻造铝合金单轴压缩下金属间颗粒裂纹损伤演化的各向异性
机译:2324-T39铝合金薄板循环载荷谱下分支裂纹疲劳裂纹扩展机理研究
机译:LY12CZ铝合金预腐蚀和疲劳裂纹行为的SEM原位研究
机译:铁和铝的近阈值疲劳裂纹扩展行为-镁合金含量为3%(裂纹关闭)。
机译:原位扫描电子显微镜观察铝合金薄板上蒸汽涂层形成的氢氧化物膜的裂纹萌生和扩展
机译:预腐蚀对铝合金裂纹萌生和疲劳寿命的影响
机译:铝合金腐蚀疲劳裂纹扩展。第一部分循环应力波形对al-Zn-mg合金腐蚀疲劳裂纹扩展的影响。第二部分。 al-Zn-mg合金腐蚀疲劳裂纹扩展机理