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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：147/42 | 提交时间：2022/07/04 |
| A Multi-space Interrelation Theory for Correlating Aerodynamic Data from Hypersonic Ground Testing 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Jiang ZL(姜宗林); Luo ZT(罗长童)
 浏览 | Adobe PDF(377Kb) | 收藏 | 浏览/下载：136/29 | 提交时间：2020/01/06 |
| A Fast Mathematical Modeling Method for Aerodynamic-Heating Predictions 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Luo ZT(罗长童); Jiang ZL(姜宗林)
浏览 | Adobe PDF(252Kb) | 收藏 | 浏览/下载：160/33 | 提交时间：2020/01/06 |
| Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
作者: Yao W(姚卫); Wu K(吴坤); Lee YC(李亚超); Fan XJ(范学军)
 Adobe PDF(1156Kb) | 收藏 | 浏览/下载：411/0 | 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; 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：298/80 | 提交时间：2018/12/26 |
| 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
作者: Wang Y; Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(1120Kb) | 收藏 | 浏览/下载：481/102 | 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：167/61 | 提交时间：2020/08/27 |
| 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
作者: 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)
浏览 | Adobe PDF(805Kb) | 收藏 | 浏览/下载：384/143 | 提交时间：2018/06/06 |
| 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
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：434/214 | 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 |
| 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：252/84 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
