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The Lift Problem in Flapping Forward Flight at Low Reynolds Numbers 会议论文
53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida, USA, Jan 1-5，2015
作者:  Liu TS;  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威)
浏览  |  Adobe PDF(1670Kb)  |  收藏  |  浏览/下载：300/86  |  提交时间：2016/01/07
On applicability of the Kutta-Joukowski theorem to low-Reynolds-number unsteady flows 会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
作者:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  Wang SZ(王士召)
浏览  |  Adobe PDF(755Kb)  |  收藏  |  浏览/下载：636/217  |  提交时间：2014/02/24
CFD for chemically reacting flow and its applications 会议论文
International Conference on Advanced Aircraft Technologies 2012, South Korea, 2012-5
作者:  Hu ZM(胡宗民);  Sun XF;  Jiang ZL(姜宗林)
Adobe PDF(1482Kb)  |  收藏  |  浏览/下载：603/144  |  提交时间：2013/03/16
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300 会议论文
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
作者:  Qi DW;  He GW(何国威);  Liu YM
Adobe PDF(738Kb)  |  收藏  |  浏览/下载：846/166  |  提交时间：2013/02/26
Aerospace Engineering  Deformation  Exhibitions  Flexible Wings  Reynolds Number  Rigidity  Vortex Flow  Aerodynamic Forces  Chord-based Reynolds Number  Flexural Rigidities  Free Stream  Free-stream Flow  Lattice Boltzmann  Leading-edge Vortices  Lift Coefficient  Lift Force  Particle Methods  Pitch Rate  Power Efficiency  Reduced Frequency  Three Dimensional Space  Time-periods  Tip Edge  Trailing Edges  Trailing Vortex  
Large-eddy simulation of flows past a flapping airfoil using immersed boundary method 会议论文
9th International Conference on Femtochemistry, Femtobiology and Femtophysics - Frontiers in Ultrafast Science and Technology (Femtochemistry IX), Beijing, PEOPLES R CHINA, AUG 08-13, 2009
作者:  Yang XL(杨晓雷);  He GW(何国威);  Zhang X(张星);  He GW
Adobe PDF(679Kb)  |  收藏  |  浏览/下载：847/174  |  提交时间：2009/07/23
Transitional Flows  Moving Boundary  Immersed Boundary Method  Smoothed Discrete Delta Function  Laminar Separation-bubbles  
Numerical Analyses of Transonic Fluid/Structure interaction in Aircraft Engineering 会议论文
Sixth World Congress on Computational Mechanics in Conjunction with the Second Asian-Pacific Congress on Computational Mechanics, Sept. 5-10, 2004, Beijing, China
作者:  Yang GW(杨国伟);  Obayashi S
Adobe PDF(1646Kb)  |  收藏  |  浏览/下载：859/243  |  提交时间：2007/12/18