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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)
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Shock  Supersonic flow  Transonic flow  
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
Authors:  Zhao C;  Yang Y(杨焱);  Zhang T;  Dong HB
Adobe PDF(1785Kb)  |  Favorite  |  View/Download：147/58  |  Submit date：2021/02/01
NUMERICAL ANALYSIS ON DRAG REDUCTION OF HIGH-SPEED TRAIN USING ROUGH SURFACE 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Yin B(银波);  Yang GW(杨国伟)
View  |  Adobe PDF(1595Kb)  |  Favorite  |  View/Download：251/54  |  Submit date：2019/04/19
EXPERIMENTAL AND NUMERICAL STUDY OF THE CLOUD CAVITATING FLOW AROUND A SLENDER CYLINDER WITH A PETALS-SHAPED SECTION 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:  Wang YW(王一伟);  Huang J(黄荐);  Xu C(徐畅);  Yu C(余超);  Huang CG(黄晨光);  Wu XC(吴小翠);  Wang, YW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.;  Wang, YW (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View  |  Adobe PDF(1600Kb)  |  Favorite  |  View/Download：403/82  |  Submit date：2018/01/16
Large-eddy Simulation  Hydrofoil  Propeller  Surface  
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors:  Gan JY;  Shen YQ(申义庆);  Zha GC
Adobe PDF(555Kb)  |  Favorite  |  View/Download：314/101  |  Submit date：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
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
Authors:  Wang SZ(王士召);  Zhang X(张星);  He GW(何国威);  Liu TS;  Wang SZ(王士召)
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A New Kinetic-Based Solver for Solving Compressible Flow on Arbitrary Polyhedral Grids 会议论文
Asia-Pacific International Symposium on Aerospace Technology, Xian, PEOPLES R CHINA, SEP 13-15, 2010
Authors:  Li SJ;  Yang GW(杨国伟);  Li, SJ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Configuration optimization of hypersonic vehicles under transitional flow conditions 会议论文
16th AIAA/DLR/DGLR International Space Planes an Hypersonic Systems and Technologies Conference, Germany, Bremen, 2009-10
Authors:  Sun QH(孙泉华);  Fan J(樊菁);  Jiang JZ(蒋建政);  Cui K(崔凯);  Sun QH(孙泉华)
Adobe PDF(377Kb)  |  Favorite  |  View/Download：1243/411  |  Submit date：2009/12/28