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Large Eddy Simulation with Sub-grid Stress Determined by Molecular Simulation and its Applications for Turbulent Channel Flows 期刊论文
Procedia Engineering, 2015, 卷号: 126, 页码: 88-92
作者:  Ceng DD(曾丹丹);  Zhong FQ(仲峰泉);  Fan J(樊菁)
浏览  |  Adobe PDF(394Kb)  |  收藏  |  浏览/下载：250/50  |  提交时间：2016/08/25
Turbulent Channel Flow  Large Eddy Simulation  Molecular Statistics  Diffusive Information Preservation  
Numerical Study of Shock/Boundary Layer Interaction of Chemically Reacting Flow in Shock Tube 期刊论文
Procedia Engineering, 2015, 卷号: 126, 页码: 617-621
作者:  Chen S(陈松);  Sun QH(孙泉华)
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载：247/95  |  提交时间：2016/08/25
Shock/boundary-layer Interaction  Nonequilibrium Chemical Reactions  Shock Tube Flow  Weno Scheme  
Monte Carlo modeling of electron density in hypersonic rarefied gas flows 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July13-18, 2014
作者:  Fan J(樊菁);  Zhang YH(张羽淮);  Jiang JZ(蒋建政)
浏览  |  Adobe PDF(835Kb)  |  收藏  |  浏览/下载：661/175  |  提交时间：2015/01/21
Hypersonic Rarefied Gas Flow  Electron Density  Dsmc  Tss  Ram-c Ii Flight Test  
Molecular simulation of small Knudsen number flows 会议论文
28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza, SPAIN, JUL 09-13, 2012
作者:  Fei F(费飞);  Fan J(樊菁);  Fei, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(476Kb)  |  收藏  |  浏览/下载：643/148  |  提交时间：2013/02/26
Dsmc  Ip  Molecular Diffusion  Time Step  Cell Size  Rarefied-gas Flows  Low-reynolds-number  Statistical Simulation  Monte-carlo  Flat-plate  Model  
Study of the coupling between real gas effects and rarefied effects on hypersonic aerodynamics 会议论文
28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza, SPAIN, JUL 09-13, 2012
作者:  Chen S(陈松);  Hu Y(胡远);  Sun QH(孙泉华);  Chen, S (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(465Kb)  |  收藏  |  浏览/下载：888/249  |  提交时间：2013/02/26
Hypersonic Flow  Real Gas Effects  Rarefied Gas Effects  Coupling Mechanism  Flow  
Molecular Motion in Isotropic Turbulence 会议论文
27th International Symposium on Rarefied Gas Dynamics, Pacific Grove, CA, JUL 10-15, 2010
作者:  Fan J(樊菁);  Jiang JZ(蒋建政);  Fei F(费飞);  Fan, J (reprint author), Chinese Acad Sci, Inst Mech, Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
Adobe PDF(326Kb)  |  收藏  |  浏览/下载：806/216  |  提交时间：2012/04/01
Isotropic Turbulence  Tracer Molecule  Tmic  Dns  Dsmc  
Monte Carlo Simulation of two-dimensional Kolmogorov flow 会议论文
27th International Symposium on Rarefied Gas Dynamics, Pacific Grove, CA, JUL 10-15, 2010
作者:  Zhang J(张俊);  Fan J(樊菁);  Zhang, J (reprint author), Chinese Acad Sci, Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China
Adobe PDF(406Kb)  |  收藏  |  浏览/下载：879/213  |  提交时间：2012/04/01
Kolmogorov Flow  Instability  Transition To Turbulence  Dsmc  
DNS of shock/boundary layer interaction flow in a supersonic compression ramp 会议论文
6th International Conference on Computational Fluid Dynamics, St Petersburg, RUSSIA, JUL 12-16, 2010
作者:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Liang X(梁贤);  Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
Adobe PDF(966Kb)  |  收藏  |  浏览/下载：696/172  |  提交时间：2013/02/26
Turbulent-boundary-layer  Direct Numerical-simulation  
One-Step Direct Aeroacoustic Simulation Using Space-Time Conservation Element and Solution Element Method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Ho CY;  Leung RCK;  Zhou K;  Lam GCY;  Jiang ZL(姜宗林)
Adobe PDF(400Kb)  |  收藏  |  浏览/下载：494/200  |  提交时间：2014/01/14
Aeroacoustics  Caa  Ce/se Method  Acoustic Wave  Supersonic Jet  
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(53Kb)  |  收藏  |  浏览/下载：784/188  |  提交时间：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy