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浏览/检索结果: 共6条，第1-6条 帮助 限定条件 发表日期：2019     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Comparative study of crack growth behaviors of fully-lamellar and bi-lamellar Ti-6Al-3Nb-2Zr-1Mo alloy 期刊论文 JOURNAL OF ALLOYS AND COMPOUNDS, 2019, 卷号: 789, 页码: 249-255 作者:  Wang, Q.;  Ren, J. Q.;  Wu, Y. K.;  Jiang, P.;  Li, J. Q. 收藏  |  浏览/下载：0/0  |  提交时间：2019/11/15 Titanium alloy  Fatigue crack growth  Lamellar structure   Comparative study of crack growth behaviors of fully-lamellar and bi-lamellar Ti-6Al-3Nb-2Zr-1Mo alloy 期刊论文 Journal of Alloys and Compounds, 2019, 卷号: 789, 页码: 249-255 作者:  Wang, Q.;  Ren, J.Q.;  Wu, Y.K.;  Jiang, P.;  Li, J.Q. 收藏  |  浏览/下载：1/0  |  提交时间：2022/02/17 Aluminum alloys  Aluminum metallography  Cracks  Fatigue crack propagation  Lamellar structures  Molybdenum alloys  Molybdenum metallography  Morphology  Niobium alloys  Niobium metallography  Titanium alloys  Titanium metallography  Zircaloy  Zirconium metallography  Alpha/beta interface  Comparative studies  Crack growth behavior  Dislocation slip  Fully lamellar  Low cycle fatigues  Secondary alpha  Surface damage morphologies   Analysis of the effect of out-of-phase biaxial fatigue loads on crack paths in cruciform specimens using XFEM 期刊论文 INTERNATIONAL JOURNAL OF FATIGUE, 2019, 卷号: 123, 页码: 87-95 作者:  Infante-Garcia D;  Qian GA(钱桂安);  Miguelez H;  Giner E 收藏  |  浏览/下载：37/0  |  提交时间：2019/05/29 XFEM  Cruciform specimen  Biaxial fatigue loading  Crack paths   Effects of microstructure on fatigue crack propagation behavior in a bi-modal TC11 titanium alloy fabricated via laser additive manufacturing 期刊论文 JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY, 2019, 卷号: 35, 页码: 403-408 作者:  Wang, Yafei;  Chen, Rui;  Cheng, Xu;  Zhu, Yanyan;  Zhang, Jikui 收藏  |  浏览/下载：7/0  |  提交时间：2019/12/30 Laser additive manufacturing  TC11 titanium alloy  Microstructure  Fatigue crack propagation path  Fatigue crack growth rate   Introduction of fretting-contact-induced crack closure: Numerical simulation of crack initiation and growth path in disk/blade attachment 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 页码: 1923-1932 作者:  Hu, Chen;  Wei, Dasheng;  Wang, Yanrong;  Jiang, Xianghua 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 Crack closure  Crack growth  Crack initiation  Finite element method  Fretting fatigue