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机译:恒定振幅载荷下航空Al-Li(2198)铝合金的疲劳行为
Department of Financial Engineering, University of the Aegean, 41 Kountouriotou Str., 82100 Chios, Greece;
Department of Financial Engineering, University of the Aegean, 41 Kountouriotou Str., 82100 Chios, Greece;
Department of Financial Engineering, University of the Aegean, 41 Kountouriotou Str., 82100 Chios, Greece;
Materials and Engineering Research Institute, Sheffield Hallam University, Howard Street, S11WB Sheffield, UK;
Aluminum alloys; Constant amplitude fatigue; Tensile properties; Fracture; Specific properties;
机译:搅拌摩擦焊接2198-T8 Al-Li合金接头的残余应力效应和疲劳行为
机译:在恒定幅度和光谱载荷下,两个铝合金的疲劳裂纹增长和裂缝闭合分析
机译:等幅和变幅载荷下7075-T651铝合金试件的疲劳和裂纹扩展分析
机译:恒定和变幅载荷下7050-T7451铝合金的疲劳和裂纹扩展
机译:在恒定和可变振幅载荷下7050-T7451铝合金的疲劳和裂纹扩展。
机译:脉冲频率对超高频脉冲交流CMT焊接获得的2198 Al-Li合金接头组织和力学性能的影响
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:铸铝合金a201-T7和a357-T6的恒载荷振幅疲劳裂纹扩展试验