Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-4 of 4 Help

Filters            
Selected(0)Clear Items/Page:    Sort:
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
Authors:  Qi DW;  He GW(何国威);  Liu YM
Adobe PDF(738Kb)  |  Favorite  |  View/Download：859/169  |  Submit date：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
Authors:  Yang XL(杨晓雷);  He GW(何国威);  Zhang X(张星);  He GW
Adobe PDF(679Kb)  |  Favorite  |  View/Download：860/178  |  Submit date：2009/07/23
Transitional Flows  Moving Boundary  Immersed Boundary Method  Smoothed Discrete Delta Function  Laminar Separation-bubbles  
An atomistic-continuum hybrid simulation of fluid flows over superhydrophobic surfaces 会议论文
Conference on Advances in Microfluidics and Nanofluidics, Hong Kong Univ Sci & Technol, Hong Kong, PEOPLES R CHINA, 2009
Authors:  Li Q(李强);  He GW(何国威);  He GW
Adobe PDF(978Kb)  |  Favorite  |  View/Download：960/149  |  Submit date：2009/07/23
Couette Flow  Flow Simulation  Molecular Dynamics Method  Navier-stokes Equations  Boundary-conditions  Molecular-dynamics  Shear-flow  Solid Interface  Slip Length  Liquid  Microchannels  Velocimetry  Roughness  Friction  
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
Authors:  Tama M;  Wang ZJ;  Rajagopalan G;  Hu H;  He GW(何国威)
Adobe PDF(4409Kb)  |  Favorite  |  View/Download：2029/716  |  Submit date：2012/02/13