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| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文 4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020 Authors: Yang L; 岳连捷 ; 张启帆 ; 张新宇![](/image/person.jpg)
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| Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation 会议论文 AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020 Authors: Jin Y ; 廖飞, Cai JS
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| Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷) ; Zhang XY(张新宇)![](/image/person.jpg)
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| Ventilated partial cavitating flow around a blunt body near the free surface 会议论文 16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016, Honolulu, HI, United states, April 10, 2016 - April 15, 2016 Authors: Wang YW(王一伟) ; Wu XC(吴小翠) ; Huang CG(黄晨光)![](/image/person.jpg)
View  |   Adobe PDF(757Kb)  |   Favorite  |  View/Download:204/42  |  Submit date:2019/11/20 Axisymmetric bodies Cavity boundaries Free surfaces High speed underwater vehicles Launching systems Media properties Unsteady behaviors Ventilated cavitation |
| 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)![](/image/person.jpg)
View  |   Adobe PDF(1377Kb)  |   Favorite  |  View/Download:306/119  |  Submit date:2020/08/26 Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Yao W(姚卫) ; Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶) ; Fan XJ(范学军) ; Fan, Xuejun(xfan@imech.ac.cn)
View  |   Adobe PDF(1173Kb)  |   Favorite  |  View/Download:481/232  |  Submit date:2018/01/16 Adiabatic Flame Temperature Aerodynamics Boundary Layer Flow Boundary Layers Chemical Analysis Combustion Computational Chemistry Directed Graphs Flow Separation Mach Number Principal Component Analysis Regression Analysis Sensitivity Analysis Spacecraft Supersonic Aerodynamics Supersonic Aircraft Transients |
| 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:449/115  |  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 |
| LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫) ; Fan XJ(范学军) ; Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
View  |   Adobe PDF(1249Kb)  |   Favorite  |  View/Download:334/101  |  Submit date:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| 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)![](/image/person.jpg)
View  |   Adobe PDF(1377Kb)  |   Favorite  |  View/Download:514/107  |  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 |
| Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Li GL(李广利) ; Cui K(崔凯) ; Xiao Y(肖尧) ; Xu YZ(徐应洲)
View  |   Adobe PDF(664Kb)  |   Favorite  |  View/Download:412/102  |  Submit date:2018/01/16 Aerodynamics Angle Of Attack Angle Of Attack Indicators Boundary Layers Drag Drag Coefficient High Pressure Effects Hypersonic Aerodynamics Hypersonic Flow Spacecraft |