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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：152/42 | 提交时间：2022/07/04 |
| Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
作者: Li B(李波); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(1358Kb) | 收藏 | 浏览/下载：152/46 | 提交时间：2021/02/01 |
| Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者: Yao W(姚卫); Chen L(陈留)
Adobe PDF(2272Kb) | 收藏 | 浏览/下载：264/145 | 提交时间：2021/06/11 |
| Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser 会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
作者: Fang SH(方思晗); Wang ZZ(王泽众); Li RJ(李仁杰); Zhang ZL(张泽林); Lin X(林鑫); Li F(李飞); Yu XL(余西龙)
Adobe PDF(1569Kb) | 收藏 | 浏览/下载：216/67 | 提交时间：2021/06/11
concentration hybrid rocket motor nozzle exit temperature Tunable diode laser absorption spectroscopy (TDLAS) water vapor |
| Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者: Yao W(姚卫); Li B(李波)
Adobe PDF(1665Kb) | 收藏 | 浏览/下载：143/43 | 提交时间：2020/11/20
Dynamic zone flamelet model GH2/GO2 Large Eddy Simulation (LES) Rocket combustor Turbulence-chemistry interaction |
| Supercritical GN2/GH2 jet modeled by the ECS method 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者: Yao W(姚卫); Jin YC(靳一超); Lee YC(李亚超)
Adobe PDF(1048Kb) | 收藏 | 浏览/下载：154/58 | 提交时间：2020/11/20 |
| 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：417/0 | 提交时间：2018/12/26 |
| 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：442/217 | 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：263/90 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, 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：329/72 | 提交时间：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
