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A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download：296/116  |  Submit date：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
View  |  Adobe PDF(1358Kb)  |  Favorite  |  View/Download：440/112  |  Submit date：2018/01/16
Computational Fluid Dynamics  Computer Software  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Runge Kutta Methods  Shock Tubes  Shock Waves  Spacecraft  Turbulence  Two Phase Flow  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
View  |  Adobe PDF(566Kb)  |  Favorite  |  View/Download：341/74  |  Submit date：2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Fast Modeling Methods for Complex System with Separable Features 会议论文
10th International Symposium on Computational Intelligence and Design (ISCID), Hangzhou, PEOPLES R CHINA, DEC 09-10, 2017
Authors:  Chen C(陈辰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
View  |  Adobe PDF(249Kb)  |  Favorite  |  View/Download：261/88  |  Submit date：2018/06/06
Data-driven Modeling  Genetic Programming  Generalized Separable Model  Multi-level Block Search  
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download：503/101  |  Submit date：2018/11/08
Computational Fluid Dynamics  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Ramjet Engines  Runge Kutta Methods  Shock Tubes  Turbulence  Two Phase Flow  Bench  Mark Problems  Central  Upwind Scheme  Computational Fluid Dynamics Software  Skew  Symmetric Forms  Temporal Discretization  Turbulence Structures  Unstructured Meshes  Wall Bounded Turbulence  
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：272/83  |  Submit date：2018/01/16
Immersed-boundary Method  Micro-air Vehicles  Insect Flight  Vortices  Forces  Flows  
Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
View  |  Adobe PDF(468Kb)  |  Favorite  |  View/Download：311/85  |  Submit date：2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics