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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
Institute of Solid Mechanics, School of Aeronautic Science and Engineering, Beihang University (BUAA), Beijing 100191, PR China;
Institute of Solid Mechanics, School of Aeronautic Science and Engineering, Beihang University (BUAA), Beijing 100191, PR China;
Institute of Solid Mechanics, School of Aeronautic Science and Engineering, Beihang University (BUAA), Beijing 100191, PR China;
Institute of Solid Mechanics, School of Aeronautic Science and Engineering, Beihang University (BUAA), Beijing 100191, PR China;
Aluminum alloy; Fatigue crack growth; Crack branching; Fracture characteristics; Crack-tip stress field;
机译:2324-T39铝合金疲劳裂纹生长路径裂纹分支机理
机译:载荷对2324-T39铝合金薄板宏观疲劳裂纹扩展路径的影响
机译:疲劳谱载荷下铝合金试件疲劳裂纹扩展速率的观察
机译:Spectrum Loading下2324-T39铝合金疲劳裂纹生长行为:实验和仿真
机译:使用压缩预裂纹测试方法在宽负荷比范围内的铝合金7050和9310钢的疲劳裂纹扩展和裂纹闭合行为
机译:铝板结构随裂纹扩展的FBG谱特征变化研究
机译:载荷谱的截断和截断对变幅载荷下7475-T7351铝合金疲劳裂纹扩展行为的影响
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