中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共4条，第1-4条 帮助

限定条件        
已选(0)清除 条数/页：   排序方式：
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  
Visualization of Vaporized Kerosene Combustion in a Supersonic Combustor Using Pulsed Schlieren System 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Atlanta, Georgia, July 30-Augest 1, 2012
作者:  Yuan YM(袁越明);  Yang M(杨猛);  Zhang TC(张泰昌);  Yu G(俞刚);  Fan XJ(范学军)
浏览  |  Adobe PDF(1965Kb)  |  收藏  |  浏览/下载：801/275  |  提交时间：2013/03/05
Mach23 的激波-平板湍流边界层干扰的直接数值模拟 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  何志伟;  李新亮
Adobe PDF(3259Kb)  |  收藏  |  浏览/下载：527/135  |  提交时间：2014/01/23
激波  湍流边界层  直接数值模拟  平均速度剖面  湍动能方程  拟序结构  压力梯度  
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