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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：249/50  |  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  
Visualization of the interaction between tris and lysozyme with a biosensor based on total internal reflection imaging ellipsometry 会议论文
6th International Conference on Spectroscopic Ellipsometry, Kyoto JAPAN, MAY 26-31 2013
作者:  Kang TF(康腾飞);  Niu Y(牛宇);  Jin G(靳刚);  gajin@imech.ac.cn
浏览  |  Adobe PDF(690Kb)  |  收藏  |  浏览/下载：395/129  |  提交时间：2015/09/29
Biosensor  Total Internal Reflection Imaging Ellipsometry  Weak Affinity Interaction  Tris  Lysozyme  
Joint detection of tumor markers with imaging ellipsometry biosensor 会议论文
6th International Conference on Spectroscopic Ellipsometry, Kyoto JAPAN, MAY 26-31 2013
作者:  Niu Y(牛宇);  Kang TF(康腾飞);  Jin G(靳刚);  gajin@imech.ac.cn
浏览  |  Adobe PDF(690Kb)  |  收藏  |  浏览/下载：423/74  |  提交时间：2015/09/29
Joint Detection  Tumor Markers  Biosensor  Imaging Ellipsometry  
Experiment study on improved closed loop pulsating heat pipe with silver/water nanofluid 会议论文
2nd International Conference on Energy and Environmental Protection (ICEEP 2013), Guilin, China, APR 19-21, 2013
作者:  Shi WX;  Li WY;  Pan LS(潘利生);  Shi, WX (reprint author), Beijing Univ Civil Engn & Architecture, Sch Environm & Energy Engn, Beijing 100044, Peoples R China.
浏览  |  Adobe PDF(428Kb)  |  收藏  |  浏览/下载：525/141  |  提交时间：2014/02/24
Nanofluid  Improved Closed Loop  Pulsating Heat Pipe  Start Up  Operation Stability  Heat Transfer  
Oscillation-free adaptive simulation of compressible two-fluid flows with different types of equation of state 会议论文
8th Workshop on Synthetic Turbulence Models, Paris, FRANCE, JUN 28-29, 2012
作者:  Zheng HW(郑洪伟);  Shu C;  Chew YT;  Qin N;  Zheng HW(郑洪伟)
Adobe PDF(972Kb)  |  收藏  |  浏览/下载：896/279  |  提交时间：2013/03/01
Compressible Multifluids  Adaptive  Equation Of State  
Numerical Simulation of a Low-power Hydrazine Arcjet Thruster 会议论文
18TH INTERNATIONAL VACUUM CONGRESS (IVC-18), Beijing, PEOPLES R CHINA, AUG 23-27, 2010
作者:  Wang HX;  Geng JY;  Chen Xi;  Pan WX(潘文霞);  Wang HX (reprint author), Beijing Univ Aeronaut & Astronaut, Sch Astronaut, Beijing 100191, Peoples R China.
Adobe PDF(212Kb)  |  收藏  |  浏览/下载：1120/334  |  提交时间：2011/01/12
Low-power Arcjet  Plasma Flow And Heat Transfer  Numerical Modeling  Hydrazine  
Fast Plasma Sintering Deposition of Nano-structured Silicon Carbide Coatings 期刊论文
Physics Procedia, 2012, 卷号: 32, 页码: 598-604
作者:  Huang HJ(黄河激);  Fu ZQ(付志强);  Pan WX(潘文霞);  Wu CK(吴承康)
浏览  |  Adobe PDF(577Kb)  |  收藏  |  浏览/下载：311/84  |  提交时间：2015/12/16
Reduced-pressure  Plasma Sintering Deposition  Silicon Carbide Coating  Ultrafast Deposition  
Detached eddy simulation for turbulent flows in a pipe with a snowflake fractal orifice 会议论文
8th Workshop on Synthetic Turbulence Models, Paris, FRANCE, JUN 28-29, 2012
作者:  Zheng HW(郑洪伟);  Nicolleau FCGA;  Qin N;  Zheng, HW (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(506Kb)  |  收藏  |  浏览/下载：550/172  |  提交时间：2013/09/17
Turbulent Flows  Dimension  Surfaces  
Hypersonic aerodynamics of a flat plate: bridging formula and wall temperature effects 会议论文
28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza, SPAIN, JUL 09-13, 2012
作者:  Hu Y(胡远);  Chen S(陈松);  Sun QH(孙泉华);  Hu, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(645Kb)  |  收藏  |  浏览/下载：883/221  |  提交时间：2013/02/26
Hypersonic Flow  Flat Plate  Bridging Formula  Dsmc Method