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	Influence of Ambient Pressure on Performance of a Deep-sea Hydraulic Manipulator 会议论文 OAI收割 Marseille, France, June 17-20, 2019 作者: Tian QY(田启岩); Zhang QF(张奇峰); Chen YZ(陈言壮); Huo LQ(霍良青); Li S(李硕) \| 收藏 \| 浏览/下载：13/0 \| 提交时间：2019/12/23 Deep-sea hydraulic manipulator Viscosity-pressure characteristics Nonlinear mathematical model 11000m on-line pressure experiment
	Analysis on velocity distribution and displacement along the profile of a slope using both empirical and analytical methods 期刊论文 OAI收割 Journal of Mountain Science, 2017, 卷号: 14, 期号: 12, 页码: 2589-2602 作者: CHEN Tie-lin; ZHOU Cheng; LIU En-long; DAI Feng; LIU Jiao \| 收藏 \| 浏览/下载：236/0 \| 提交时间：2017/12/07 Slope Deformation Progressive Deformation Fitting Function Analytical Solution Bingham Model Nonlinear Viscosity
	Vanishing viscosity of isentropic Navier-Stokes equations for interacting shocks 期刊论文 OAI收割 SCIENCE CHINA-MATHEMATICS, 2015, 卷号: 58, 期号: 4, 页码: 653-672 作者: Huang FeiMin; Wang Yi; Wang Yong; Yang Tong \| 收藏 \| 浏览/下载：120/0 \| 提交时间：2021/01/14 NONLINEAR HYPERBOLIC SYSTEMS ZERO-DISSIPATION LIMIT CONSERVATION-LAWS RAREFACTION WAVES EULER EQUATIONS BOLTZMANN-EQUATION CONVERGENCE RATE GAS-DYNAMICS APPROXIMATIONS STABILITY isentropic Navier-Stokes equations isentropic Euler equations interacting shock vanishing viscosity entropy solution
	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.
	Applications of urans on predicting unsteady turbulent separated flows 期刊论文 iSwitch采集 Acta mechanica sinica, 2009, 卷号: 25, 期号: 3, 页码: 319-324 作者: Xu, Jinglei; Ma, Huiyang 收藏 \| 浏览/下载：31/0 \| 提交时间：2019/05/10 Urans Nonlinear eddy viscosity turbulence model Separated flows Circular cylinder
	Nonlinear turbulence models for predicting strong curvature effects 期刊论文 iSwitch采集 Applied mathematics and mechanics-english edition, 2008, 卷号: 29, 期号: 1, 页码: 31-42 作者: Xu Jing-lei; Ma Hui-yang; Huang Yu-ning 收藏 \| 浏览/下载：24/0 \| 提交时间：2019/05/10 Curvature effect Nonlinear eddy viscosity turbulence model Reynolds stress model
	Fully nonlinear parabolic equations and the Dini condition 期刊论文 OAI收割 ACTA MATHEMATICA SINICA-ENGLISH SERIES, 2002, 卷号: 18, 期号: 3, 页码: 473-480 作者: Zou, X; Chen, YZ \| 收藏 \| 浏览/下载：12/0 \| 提交时间：2018/07/30 fully nonlinear uniformly parabolic equations viscosity solutions Dini condition
	Viscosity solution to nonlinear H-infinity control 期刊论文 OAI收割 CHINESE SCIENCE BULLETIN, 1997, 卷号: 42, 期号: 11, 页码: 890-894 作者: Hong, YG; Yung, SP; Mei, SW; Qin, HS \| 收藏 \| 浏览/下载：11/0 \| 提交时间：2018/07/30 nonlinear H infinity control viscosity solution disturbance attenuation