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机译:拉应力作用下压应力对疲劳裂纹扩展的影响
Composite Materials and Structure Research Centre, Harbin Institute of Technology, Harbin 150001, People's Republic of China;
Composite Materials and Structure Research Centre, Harbin Institute of Technology, Harbin 150001, People's Republic of China;
School of Mechanical and Power Engineering, Harbin University of Science and Technology, Harbin 150080, People's Republic of China;
Composite Materials and Structure Research Centre, Harbin Institute of Technology, Harbin 150001, People's Republic of China;
crack propagation; compressive loading; strain hardening; fatigue crack closure; finite element analysis;
机译:同期和异相混合模式加载:由于张力 - 压缩和扭转载荷,森标本疲劳裂纹生长的研究
机译:高压缩载荷对冷扩孔残余应力和疲劳裂纹扩展的影响
机译:压缩载荷和裂纹闭合对负载荷比疲劳纯钛疲劳裂纹生长的影响
机译:空气中张力压缩载荷下低合金钢疲劳裂纹生长
机译:使用紧凑和双缺口缺口拉伸压缩试样在蠕变疲劳条件下的裂纹扩展行为。
机译:拉伸-拉伸拉伸-压缩和压缩-压缩疲劳载荷下增材制造的Ti6Al4V支架的疲劳寿命
机译:高标称应力和低标称应力下疲劳裂纹生长规律的比较:退火0.45%C钢的完全反转拉伸压缩
机译:飞机结构的结构完整性分析和验证:第2卷:压缩载荷对7075-T651和2024-T3铝合金疲劳裂纹扩展速率的影响