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CORC

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Semi-parametric inference for semi-varying coefficient panel data model with individual effects 期刊论文
JOURNAL OF MULTIVARIATE ANALYSIS, 2017, 卷号: 154, 页码: 262-281
作者:  Hu, Xuemei
收藏  |  浏览/下载：16/0  |  提交时间：2018/07/30
Hydrodynamic effects on the surface morphology evolution of aluminum alloy under intense pulsed ion beam irradiation 会议论文
20th International Conference on Ion Beam Modification of Materials (IBMM), Wellington, NEW ZEALAND, 2017-10-15
作者:  Yu, Xiao;  Zhong, Haowen;  Zhang, Zhou;  Shen, Jie;  Zhang, Jie
收藏  |  浏览/下载：6/0  |  提交时间：2019/12/30
Hydrodynamic effects on the surface morphology evolution of aluminum alloy under intense pulsed ion beam irradiation 期刊论文
20th International Conference on Ion Beam Modification of Materials (IBMM), 2017, 卷号: 409, 页码: 158-162
作者:  Yu, Xiao;  Zhong, Haowen;  Zhang, Zhou;  Shen, Jie;  Zhang, Jie
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/30
Nonparametric estimation of conditional VaR and expected shortfall 期刊论文
http://www.wise.xmu.edu.cn/paperInfor.asp?id=123, 2013
Zongwu Cai; Xian Wang
收藏  |  浏览/下载：10/0  |  提交时间：2013/11/08
A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文
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：63/0  |  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.  
A score test for variance components in a semiparametric mixed-effects model under non-normality 期刊论文
STATISTICS AND ITS INTERFACE, 2011, 卷号: 4, 期号: 1, 页码: 65-72
作者:  Sun, Yan;  Zhang, Jin-Ting
收藏  |  浏览/下载：2/0  |  提交时间：2019/08/22
Techniques to improve the accuracy of noise power spectrum measurements in digital x‐ray imaging based on background trends removal 期刊论文
Medical Physics, 2011, 卷号: Vol.38 No.3, 页码: 1600-1610
作者:  Zhou, Z.a,b;  Gao, F.a,b;  Zhao, H.a,b;  Zhang, L.a,b
收藏  |  浏览/下载：1/0  |  提交时间：2019/11/26
The study of two FOG filter methods in improving the precision of servo control system (EI CONFERENCE) 会议论文
2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010, August 20, 2010 - August 22, 2010, Chengdu, China
Zhang Y.; Zhang S.-M.; Liu X.; Zhang L.-G.
收藏  |  浏览/下载：14/0  |  提交时间：2013/03/25
ANOVA FOR LONGITUDINAL DATA WITH MISSING VALUES 其他
2010-01-01
Chen, Song Xi; Zhong, Ping-Shou
收藏  |  浏览/下载：6/0  |  提交时间：2015/11/13
Well-posedness of Cauchy problem for the fourth order nonlinear Schrodinger equations in multi-dimensional spaces 期刊论文
JOURNAL OF MATHEMATICAL ANALYSIS AND APPLICATIONS, 2007, 卷号: 328, 期号: 1, 页码: 58-83
作者:  Hao, Chengchun;  Hsiao, Ling;  Wang, Baoxiang
收藏  |  浏览/下载：11/0  |  提交时间：2018/07/30

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