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浏览/检索结果: 共9条,第1-9条 帮助

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LARGE-TIME BEHAVIORS OF THE SOLUTION TO 3D COMPRESSIBLE NAVIER-STOKES EQUATIONS IN HALF SPACE WITH NAVIER BOUNDARY CONDITIONS 期刊论文  OAI收割
COMMUNICATIONS ON PURE AND APPLIED ANALYSIS, 2021, 卷号: 20, 期号: 7-8, 页码: 2811-2838
作者:  
Wang, T. E. N. G.;  Wang, Y., I
  |  收藏  |  浏览/下载:37/0  |  提交时间:2021/10/26
Regularity Criteria for Navier-Stokes Equations with Slip Boundary Conditions on Non-flat Boundaries via Two Velocity Components 期刊论文  OAI收割
ADVANCES IN NONLINEAR ANALYSIS, 2019, 卷号: 9, 期号: 1, 页码: 633-643
作者:  
da Veiga HB;  Yang JQ(杨佳琦)
  |  收藏  |  浏览/下载:23/0  |  提交时间:2019/09/09
Galilean invariant fluid-solid interfacial dynamics in lattice Boltzmann simulations 期刊论文  OAI收割
JOURNAL OF COMPUTATIONAL PHYSICS, 2014, 卷号: 266, 页码: 161—170
Wen, BH; Zhang, CY; Tu, YS; Wang, CL; Fang, HP
收藏  |  浏览/下载:30/0  |  提交时间:2015/03/13
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.  
An Atomistic-Continuum Hybrid Simulation Of Fluid Flows Over Superhydrophobic Surfaces 期刊论文  OAI收割
Biomicrofluidics, 2009
作者:  
Li Q(李强);  He GW(何国威)
收藏  |  浏览/下载:1333/338  |  提交时间:2009/08/03
An atomistic-continuum hybrid simulation of fluid flows over superhydrophobic surfaces 会议论文  OAI收割
Conference on Advances in Microfluidics and Nanofluidics, Hong Kong Univ Sci & Technol, Hong Kong, PEOPLES R CHINA, 2009
作者:  
He GW(何国威)
收藏  |  浏览/下载:750/132  |  提交时间:2009/07/23
Vanishing viscous limits for the 2D lake equations with Navier boundary conditions 期刊论文  OAI收割
JOURNAL OF MATHEMATICAL ANALYSIS AND APPLICATIONS, 2008, 卷号: 338, 期号: 2, 页码: 1070-1080
作者:  
Jiu, Quansen
  |  收藏  |  浏览/下载:18/0  |  提交时间:2018/07/30
The initial boundary value problem for Navier-Stokes equations 期刊论文  OAI收割
ACTA MATHEMATICA SINICA-ENGLISH SERIES, 1999, 卷号: 15, 期号: 2, 页码: 153-164
作者:  
He, C
  |  收藏  |  浏览/下载:17/0  |  提交时间:2018/07/30