...
机译:在概率寿命预测中纳入小的疲劳裂纹扩展:Ti-6Al-2Sn-4Zr-6Mo中应力比的影响
U.S. Air Force Research Laboratory, Materials and Manufacturing Directorate. AFRL/RXCM, Wright-Patterson Air Force Base, OH 45433, United States;
Universal Technology Corporation, Dayton, OH 45432. United States;
U.S. Air Force Research Laboratory, Materials and Manufacturing Directorate. AFRL/RXCM, Wright-Patterson Air Force Base, OH 45433, United States;
U.S. Air Force Research Laboratory, Materials and Manufacturing Directorate. AFRL/RXCM, Wright-Patterson Air Force Base, OH 45433, United States;
small fatigue crack; stress ratio; Ti-6Al-2Sn-4Zr-6Mo; life prediction;
机译:基于三维有限元法的应力集中部位表面裂纹疲劳裂纹扩展寿命预测
机译:Ti-6Al-2Sn-4Zr-6Mo的双重疲劳失效模式及其对概率寿命预测的影响
机译:铸造Al-Si-Mg合金的疲劳裂纹扩展特征。第二部分使用疲劳裂纹扩展数据进行寿命预测
机译:高循环疲劳光谱下合金Ti-6A-2Sn-4ZR-6MO寿命预测阈值疲劳裂纹裂纹裂纹裂纹裂纹的作用
机译:时效硬化不锈钢的疲劳裂纹萌生和表面损伤的检测(微裂纹密度,生长速率,光学相关性,疲劳寿命预测)
机译:线性弹性材料疲劳裂纹生长路径和寿命预测的数值分析
机译:裂纹生长预测降低循环疲劳的损伤评估(循环热应力下的疲劳寿命)
机译:在概率寿命预测中结合小疲劳裂纹扩展:应力比在Ti-6al-2sn-4Zr-6-mo(预印刷)中的影响。