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Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1120Kb)  |  Favorite  |  View/Download:84/14  |  Submit date:2018/12/26
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
View  |  Adobe PDF(805Kb)  |  Favorite  |  View/Download:132/34  |  Submit date:2018/06/06
THE MECHANISM OF THREE-DIMENSION STEADY SHOCK WAVE INTERACTION 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Wang C(王春);  Yang RX(杨瑞欣);  Jiang ZL(姜宗林)
View  |  Adobe PDF(3021Kb)  |  Favorite  |  View/Download:33/8  |  Submit date:2019/04/19
Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion 会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
Authors:  Liu CY;  Zhang J(张健)
View  |  Adobe PDF(414Kb)  |  Favorite  |  View/Download:38/9  |  Submit date:2018/11/08
Oxygen  Diluted environments  Monotonic trend  Partial premixing  Stabilization mechanisms  Transition process  Transitional flames  Transitional process  Turbulent combustion  
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:115/36  |  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  
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download:121/25  |  Submit date:2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
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:112/14  |  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  
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
Authors:  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.
View  |  Adobe PDF(3818Kb)  |  Favorite  |  View/Download:86/21  |  Submit date:2018/01/16
Concave Surface Curvature  Adverse Pressure-gradient  Large-eddy Simulation  Reynolds-number  Near-wall  Flows  Separation  Vortices  Models  
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:86/19  |  Submit date:2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
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:89/7  |  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