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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:110/35  |  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  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
View  |  Adobe PDF(735Kb)  |  Favorite  |  View/Download:92/25  |  Submit date:2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
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:117/25  |  Submit date:2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
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:80/17  |  Submit date:2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)  |  Favorite  |  View/Download:657/214  |  Submit date:2013/09/21
Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models  
Experimental and computational investigation of a full aircraft flutter at transonic speeds 会议论文
International Forum on Aeroelasticity and Structural Dynamics, IFASD 2013, Bristol, United kingdom, June 24, 2013 - June 27, 2013
Authors:  Qian W;  Yang GW(杨国伟);  Luo JG;  Yang R;  Zhang GJ
Favorite  |  View/Download:9/0  |  Submit date:2018/11/08
Aeroelasticity  Aircraft manufacture  Airframes  Computational fluid dynamics  Elastic waves  Flutter (aerodynamics)  Structural dynamics  Supersonic aircraft  Transonic aerodynamics  Viscous flow  Wind stress  Wind tunnels  Aircraft structure  CFD simulations  CFD/CSD  Computational investigation  Flutter boundary predictions  Transonic flutter  Unsteady aerodynamics  Wind tunnel tests