机译:选择性变幅载荷下纤维金属层板的疲劳裂纹扩展
Aerospace Materials and Structures, Faculty of Aerospace Engineering, Delft University of Technology, P. O. Box 50 58, 2600 GB Delft, The Netherlands;
Aerospace Materials and Structures, Faculty of Aerospace Engineering, Delft University of Technology, P. O. Box 50 58, 2600 GB Delft, The Netherlands;
Aerospace Materials and Structures, Faculty of Aerospace Engineering, Delft University of Technology, P. O. Box 50 58, 2600 GB Delft, The Netherlands;
Aerospace Materials and Structures, Faculty of Aerospace Engineering, Delft University of Technology, P. O. Box 50 58, 2600 GB Delft, The Netherlands;
crack closure; crack growth; fatigue; fibre metal laminates; GLARE; selective variable-amplitude fatigue;
机译:张力和销钉载荷下纤维金属层压板疲劳裂纹扩展行为的预测方法
机译:改进的Wheeler模型在预测可变振幅载荷下纤维金属层压板疲劳裂纹扩展中的应用
机译:通过比较开裂应力数据验证延性载荷下延性合金疲劳裂纹扩展的状态空间模型
机译:销载荷对纤维金属层压板疲劳裂纹生长的试验研究
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:各种可植入金属的疲劳特性和疲劳裂纹扩展速率的比较
机译:销钉载荷对纤维金属层板疲劳裂纹扩展影响的实验研究
机译:恒定和变幅载荷下的疲劳与疲劳裂纹扩展分析