机译:一种估算Ti-6Al-4V部件疲劳缺口因子的新方法
Department of Mechanical Engineering, Howard University, Washington, DC 20059, USA;
Department of Mechanical Engineering, Howard University, Washington, DC 20059, USA;
Department of Mechanical Engineering, Howard University, Washington, DC 20059, USA;
Department of Mechanical Engineering, Howard University, Washington, DC 20059, USA;
Weakest link; Fatigue notch factor; Titanium alloy; Closed-from solutions;
机译:评估缺口结构构件疲劳裂纹萌生和扩展寿命的两阶段方法
机译:一种估算可变振幅疲劳载荷下缺口部件寿命的弹塑性方法:初步研究
机译:估算带缺口构件在单轴和多轴循环载荷下的高周疲劳强度的统一方法
机译:缺口材料疲劳强度图的制定:思考估算缺口尺寸效应的因素
机译:估算与微结构有关的疲劳缺口因子的极值概率方法
机译:羟基磷灰石涂层Ti-6Al-4V缺口件的耐磨性和疲劳行为研究
机译:升高温度下Ti-6Al-4V合金中射击喷丸组分的疲劳性能。
机译:缺口和无缺口退火Ti-6al-4V板的恒定振幅疲劳寿命数据