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Parametric study on wing-lambda-shock formation 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
作者:  Chainok S;  Rungroch T;  Chairach P;  Prapamonthon P;  Yooyen S;  Yin B(银波);  Yang GW(杨国伟);  Ju SJ(鞠胜军)
Adobe PDF(3026Kb)  |  收藏  |  浏览/下载：270/86  |  提交时间：2021/11/30
Shock  Supersonic flow  Transonic flow  
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions 会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
作者:  Prapamonthon P;  Yin B(银波);  Yang GW(杨国伟);  Zhang MH(张莫晗)
Adobe PDF(2782Kb)  |  收藏  |  浏览/下载：158/60  |  提交时间：2020/11/20
Aerothermal condition  Cooling effectiveness  Cooling performance  Thermal sensitivity  Turbine vane  
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
作者:  Tong FL(童福林);  Li XL(李新亮);  Duan, Yanhui;  Yu ZP(于长平);  Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(3818Kb)  |  收藏  |  浏览/下载：294/117  |  提交时间：2018/01/16
Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
Experimental and computational investigation of a full aircraft flutter at transonic speeds 会议论文
International Forum on Aeroelasticity and Structural Dynamics, IFASD 2013, Bristol, United kingdom, June 24, 2013 - June 27, 2013
作者:  Qian W;  Yang GW(杨国伟);  Luo JG;  Yang R;  Zhang GJ
收藏  |  浏览/下载：151/0  |  提交时间：2018/11/08
Aeroelasticity  Aircraft manufacture  Airframes  Computational fluid dynamics  Elastic waves  Flutter (aerodynamics)  Structural dynamics  Supersonic aircraft  Transonic aerodynamics  Viscous flow  Wind stress  Wind tunnels  Aircraft structure  CFD simulations  CFD/CSD  Computational investigation  Flutter boundary predictions  Transonic flutter  Unsteady aerodynamics  Wind tunnel tests  
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：836/161  |  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  
Spanwise stretching and collapse motions stabilize leading-edge vortex in slow-flying bats 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
作者:  Wang SZ(王士召);  He GW(何国威);  Zhang X(张星)
Adobe PDF(361Kb)  |  收藏  |  浏览/下载：406/110  |  提交时间：2014/04/02
Stretching  Stabilize  Flying  Leading  Collapse  Vortex  Oscillating  Stable  Slowing  Still  Simulate  Observed  Morphology  Around  Motion  Where  Taken  Method  Study  
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：1776/1222  |  提交时间：2013/03/01
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：885/247  |  提交时间：2013/02/26
Hypersonic Flow  Real Gas Effects  Rarefied Gas Effects  Coupling Mechanism  Flow  
基于混合网格NS 方程并行计算的某机全机颤振特性分析 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  郑冠男;  杨国伟;  钱卫
Adobe PDF(569Kb)  |  收藏  |  浏览/下载：414/136  |  提交时间：2014/01/23
Cfd  Csd  气动弹性  耦合算法  颤振特性  Mpi  
基于降阶模型的叶片失谐颤振分析 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  张陈安;  张伟伟;  叶正寅;  王发民
Adobe PDF(591Kb)  |  收藏  |  浏览/下载：523/174  |  提交时间：2014/01/23
叶轮机械  颤振  失谐  气动阻尼  降阶模型