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Numerical simulation of acoustic scattering and flow-induced noise with sharp interface immersed boundary method 会议论文
AIAA Scitech 2020 Forum, Orlando, FL, 2020/1/6-10
作者:  Zhao C;  Yang Y(杨焱);  Zhang T;  Dong HB
Adobe PDF(1785Kb)  |  收藏  |  浏览/下载：116/48  |  提交时间：2021/02/01
INVESTIGATION OF OBSTACLE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF FLAPPING WINGS 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
作者:  Yin B(银波);  Yang GW(杨国伟);  Yin, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
浏览  |  Adobe PDF(6552Kb)  |  收藏  |  浏览/下载：251/77  |  提交时间：2018/01/16
Immersed-boundary Method  Micro-air Vehicles  Insect Flight  Vortices  Forces  Flows  
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：298/86  |  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：630/214  |  提交时间：2014/02/24
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：840/163  |  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  
Intrinsic lengths govern failure mode transition in metallic glasses 会议论文
ICTAM, 北京, 2012-8
作者:  Dai LH(戴兰宏);  Chen Y(陈艳)
Adobe PDF(691Kb)  |  收藏  |  浏览/下载：1780/1224  |  提交时间：2013/03/01
Aerodynamic Performance of a Corrugated Dragonfly Airfoil Compared with Smooth Airfoils at Low Reynolds Numbers 会议论文
45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2007-1-8~2007-1-11
作者:  Tama M;  Wang ZJ;  Rajagopalan G;  Hu H;  He GW(何国威)
Adobe PDF(4409Kb)  |  收藏  |  浏览/下载：2007/712  |  提交时间：2012/02/13