机构

• 金属研究所 [1]
• 地理科学与资源研究所 [1]
• 长春光学精密机械与物... [1]
• 自动化研究所 [1]

采集方式

• OAI收割 [4]

内容类型

• 期刊论文 [2]
• SCI/SSCI论文 [1]
• 会议论文 [1]

发表日期

• 2023 [1]
• 2018 [1]
• 2011 [1]
• 2009 [1]

学科主题

• Materials ... [1]
• Metallurgy... [1]

筛选

浏览/检索结果: 共4条，第1-4条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Probabilistic Boundary-Guided Point Cloud Primitive Segmentation Network 期刊论文  OAI收割 IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2023, 卷号: 72, 页码: 13 作者:  Wang, Shaohu;  Qin, Fangbo;  Tong, Yuchuang;  Shang, Xiuqin;  Zhang, Zhengtao   |  收藏  |  浏览/下载：14/0  |  提交时间：2023/12/21 Boundary prediction  primitive segmentation  probabilistic representation   Atomic-scale observation and analysis of chemical ordering in M3B2 and M5B3 borides 期刊论文  OAI收割 ACTA MATERIALIA, 2018, 卷号: 149, 页码: 274-284 作者:  Hu, XB;  Niu, HY;  Ma, XL;  Oganov, AR;  Fisher, CAJ   |  收藏  |  浏览/下载：57/0  |  提交时间：2018/06/05 Crystal-structure Prediction  Total-energy Calculations  Nickel-base Superalloys  Ni-based Superalloy  X-ray Spectroscopy  Wave Basis-set  Probe Tomography  Polycrystalline Superalloy  Grain-boundary  Resolution   A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文  OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏  |  浏览/下载：67/0  |  提交时间：2013/03/25 In this paper  a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime  but not accurate enough in the supersonic regime. 2011 IEEE.   Modelling the impacts of weather and climate variability on crop productivity over a large area: A new process-based model development, optimization, and uncertainties analysis SCI/SSCI论文  OAI收割 2009 作者:  Zhang Z. 收藏  |  浏览/下载：42/0  |  提交时间：2012/06/08 Agriculture  Climate change  CO(2) fertilization effects  Transpiration  Water use efficiency  Yield prediction  rising co2 concentrations  elevated carbon-dioxide  light-use  efficiency  stomatal conductance  water-use  terrestrial biosphere  atmospheric co2  boundary-layer  yield  photosynthesis