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浏览/检索结果: 共5条，第1-5条 帮助 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 First-principles theoretical and experimental studies of effects of ruthenium on precipitation behavior of μ phase and μ/matrix interface stability in Ni-based single crystal superalloys 期刊论文 Intermetallics, 2019, 卷号: 113 作者:  Jin H.;  Zhang J.;  Zhang Y.;  Zhang W.;  Li P. 收藏  |  浏览/下载：10/0  |  提交时间：2019/12/11 A. Intermetallics  B. Density functional theory  B. Diffusion  B. Nucleation and growth  D. Interfaces  G. aero-engine components   A multi-axial low-cycle fatigue life prediction model considering effects of additional hardening 期刊论文 FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2018, 卷号: 41, 期号: 7, 页码: 1488-1503 作者:  Zhao, B. F.;  Xie, L. Y.;  Bai, X.;  Ren, J. G.;  Li, H. Y. 收藏  |  浏览/下载：26/0  |  提交时间：2021/02/02 additional hardening  critical plane approach  fatigue life prediction  multi-axial fatigue  non-proportional loading   A Complexity-Based Approach to Robust Design and Structural Assessment of Aero Engine Components 会议论文 ASME:Structures & Dynamics: Probabilistic Methods and Applications, 2007 D. Lomario, G. P. De Poli, L. Fattore, and J. Marczyk 收藏  |  浏览/下载：8/0  |  提交时间：2011/11/28 A Complexity-Based Approach to Robust Design and Structural Assessment of Aero Engine Components 会议论文 2007 D. Lomario, G. P. De Poli, L. Fattore, and J. Marczyk 收藏  |  浏览/下载：13/0  |  提交时间：2011/11/28 Analysis of superalloy turbine blade tip cracking during service 期刊论文 Engineering Failure Analysis, 2006, 卷号: 13, 期号: 8, 页码: 1429-1436 Y. J. Xie; M. C. Wang; G. Zhang; M. Chang 收藏  |  浏览/下载：17/0  |  提交时间：2012/04/14 turbine blade tip  crack  corrosion  thermal stress  failure analysis