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Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载:36/14  |  提交时间:2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
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, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  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)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:59/21  |  提交时间: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, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
浏览  |  Adobe PDF(1358Kb)  |  收藏  |  浏览/下载:51/9  |  提交时间: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, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(566Kb)  |  收藏  |  浏览/下载:60/11  |  提交时间:2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
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, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载:45/12  |  提交时间:2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载:32/11  |  提交时间:2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
浏览  |  Adobe PDF(468Kb)  |  收藏  |  浏览/下载:47/12  |  提交时间:2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics  
Numerical study of oblique detonation initiations with chain-branching kinetics 会议论文
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, 9-13 January 2017
作者:  Teng HH(滕宏辉);  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
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Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
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Spacecraft  
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, Hypersonics 2017, Xiamen, China, 6-9 March 2017
作者:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载:69/15  |  提交时间:2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis