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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
作者:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  收藏  |  浏览/下载：151/42  |  提交时间：2022/07/04
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Li B;  Lee YC(李亚超);  Yao W(姚卫);  Lu Y(陆阳);  Fan XJ(范学军)
浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：305/82  |  提交时间：2018/12/26
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018
作者:  Li B(李波);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：173/64  |  提交时间：2020/08/27
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
作者:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：279/113  |  提交时间：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
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：423/107  |  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  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, 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：260/89  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
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
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：480/91  |  提交时间：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  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：274/81  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(590Kb)  |  收藏  |  浏览/下载：364/92  |  提交时间：2017/05/05
Frequency Spectrum Analysis  High Temporal Resolution  Instantaneous Flow  Noise Generation Mechanisms  Theoretical Modeling  Three  Dimensional Numerical Studies  Transport Mechanism  Under  Expanded Jets  
Blowout limits of supercritical kerosene in supersonic combustors 会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
作者:  Zhang TC(张泰昌);  Wang J(王晶);  Yuan YM(袁越明);  Li JG(李建国);  Yu G(俞刚);  Fan XJ(范学军);  Zhang TC(张泰昌)
浏览  |  Adobe PDF(619Kb)  |  收藏  |  浏览/下载：587/187  |  提交时间：2014/02/24