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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
Authors:  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)  |  Favorite  |  View/Download：289/93  |  Submit date：2021/11/30
Shock  Supersonic flow  Transonic flow  
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
Authors:  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.
View  |  Adobe PDF(6552Kb)  |  Favorite  |  View/Download：263/81  |  Submit date：2018/01/16
Immersed-boundary Method  Micro-air Vehicles  Insect Flight  Vortices  Forces  Flows  
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds 会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
Authors:  Qian W;  Yang GW(杨国伟);  Zheng GN(郑冠男);  Zhang GJ
View  |  Adobe PDF(1159Kb)  |  Favorite  |  View/Download：211/70  |  Submit date：2017/05/27
All-movable Horizontal Tail  Flutter Boundaries  Overload Factors  Structure Dynamics  Transonic Flutter  Transonic Speed  Wind Tunnel Tests  Wind-tunnel Testing  
Comparisons of high order hybrid schemes using a parameter-free discontinuity detector 会议论文
42nd AIAA Fluid Dynamics Conference and Exhibit 2012, New Orleans, LA, United states, JUN 25-28, 2012
Authors:  Shen YQ(申义庆);  Zha GC;  Yang GW(杨国伟);  Gao Z(高智);  Shen YQ(申义庆)
View  |  Adobe PDF(2531Kb)  |  Favorite  |  View/Download：489/109  |  Submit date：2014/02/24
双旁侧进气高超声速飞机气动布局与评估 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:  胡守超;  崔凯;  李广利;  屈志朋;  杨国伟
Adobe PDF(1737Kb)  |  Favorite  |  View/Download：515/134  |  Submit date：2014/01/23
高超声速  双旁侧进气  气动布局  计算流体动力学(Cfd)  
Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟)
View  |  Adobe PDF(199Kb)  |  Favorite  |  View/Download：479/75  |  Submit date：2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ  
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(53Kb)  |  Favorite  |  View/Download：828/191  |  Submit date：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Optimization of the upper surface of hypersonic vehicle based on CFD analysis 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Gao TY(高太元);  Cui K(崔凯);  Hu SC(胡守超);  Wang XP(王秀平);  Yang GW(杨国伟);  Gao, TY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(305Kb)  |  Favorite  |  View/Download：731/199  |  Submit date：2013/02/26
Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)  
基于CFD分析的高超声速飞行器上表面优化 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  高太元;  崔凯;  胡守超;  王秀平;  杨国伟
Adobe PDF(609Kb)  |  Favorite  |  View/Download：621/199  |  Submit date：2014/01/23
高超声速  B-样条参数化  Sqp  Cfd  
双发动机高超声速乘波飞行器性能分析 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:  崔凯;  高太元;  胡守超;  王秀平;  杨国伟
Adobe PDF(873Kb)  |  Favorite  |  View/Download：544/170  |  Submit date：2014/01/23
高超声速  乘波体  升阻比  计算流体力学