Alloys; Fracture(Mechanics); Bomber aircraft; Aluminum alloys; Titanium alloys; Steel; Nickel alloys; Cobalt alloys; Corrosion resistant alloys; Heat treatment; Grain structures(Metallurgy); Welds; Diffusion bonding; Fatigue(Mechanics); Crack propagation; Test facilities; Test methods; B-1 aircraft; Aluminum alloy 2024; Aluminum alloy 2124; Aluminum alloy 2219; Aluminum alloy 7049; Aluminum alloy 7050; Aluminum alloy 7075; Aluminum alloy 7175; Titanium alloy 6Al 4V; Steel 9Ni 4Co .2C; Steel 9Ni 4Co .3C; Steel 300M; Steel PH13-8Mo; Nickel alloy Inconel 718; Cobalt alloy MP35N;
机译:焊接接头行为评估中断裂力学参数与疲劳裂纹扩展参数的相容性
机译:评估热老化对硫化天然橡胶疲劳裂纹扩展影响的断裂力学方法
机译:用断裂力学和渐进损伤方法对胶接接头疲劳损伤和裂纹扩展的预测比较
机译:预测与观察到的疲劳裂纹扩展:北海夹克疲劳的概率断裂力学分析的验证
机译:线性弹性断裂力学预测对冷扩孔一维和二维疲劳裂纹扩展的评估。
机译:用断裂力学和分形术分析牙科陶瓷亚临界裂纹的扩展
机译:缺口构件中的初始疲劳裂纹扩展行为(报告II):用弹塑性断裂力学(力学,强度和结构设计)评估缺口场中的疲劳裂纹