Institue of Aircraft Design and Lightweight Structures,TU Braunschweig,Hermann-Blenk-Strasse 35,38108 Braunschweig,Germany;
Institue of Aircraft Design and Lightweight Structures,TU Braunschweig,Hermann-Blenk-Strasse 35,38108 Braunschweig,Germany;
Institue of Aircraft Design and Lightweight Structures,TU Braunschweig,Hermann-Blenk-Strasse 35,38108 Braunschweig,Germany;
Institue of Aircraft Design and Lightweight Structures,TU Braunschweig,Hermann-Blenk-Strasse 35,38108 Braunschweig,Germany;
Institue of Aircraft Design and Lightweight Structures,TU Braunschweig,Hermann-Blenk-Strasse 35,38108 Braunschweig,Germany;
composite; fatigue; defects; large strains; very high cycle fatigue;
机译:具有拉伸平均应变效应的SiC颗粒增强Al-Si铸造合金复合材料的低周疲劳寿命
机译:一种新的基于应变能密度的疲劳准则,该准则考虑了平均应力和塑性对平面和缺口构件的中到高周期单轴疲劳强度的影响
机译:不同应变率下拉伸弹性预变形对SAE 1050钢高周疲劳行为的影响及疲劳寿命预测
机译:复合疲劳:缺陷的影响,大应变和非常高的循环疲劳
机译:腐蚀疲劳的Aluminum-2024-T4和疲劳的钛-6铝-4钒合金的缺陷组织分析。
机译:基于创新的J2-Flow弹塑性模型的金属基复合材料低周疲劳疲劳破坏效应仿真
机译:设计用于HCF(高循环疲劳)和LCF(低循环疲劳)的测试棒的合适形状,并消除内部缺陷以减少其影响