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| Reconstruction model for heat release rate based on artificial neural network 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 37, 页码: 19599-19616 作者: Li B(李波); Yao W(姚卫); Li YC(李亚超); Fan XJ(范学军) Adobe PDF(5169Kb)  |  收藏  |  浏览/下载:101/25  |  提交时间:2022/10/25 Heat release rate (HRR) Artificial neural network (ANN) Proper orthogonal -12omposition (POD) Chemiluminescence Supersonic hydrogen flame |
| 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:150/45  |  提交时间:2021/02/01 |
| 不同喷压比下欠膨胀射流对特征频率激励的响应 期刊论文 推进技术, 2019, 卷号: 40, 期号: 06, 页码: 1239-1246 作者: 李晓鹏; 周蕊; 庄法坤; 曹逻炜; 谢国山; 范学军 浏览  |  Adobe PDF(6645Kb)  |  收藏  |  浏览/下载:365/49  |  提交时间:2019/09/12 欠膨胀射流 喷压比 特征频率激励 大涡模拟 流动响应 |
| Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文 JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465 作者: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军) Adobe PDF(862Kb)  |  收藏  |  浏览/下载:321/97  |  提交时间:2019/04/11 |
| 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:414/0  |  提交时间:2018/12/26 |
| Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文 JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991 作者: Yao W(姚卫); Lu Y(陆阳); Wu K(吴坤); Wang J(王晶); Fan XJ(范学军) Adobe PDF(2427Kb)  |  收藏  |  浏览/下载:353/106  |  提交时间:2018/10/19 |
| Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文 ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350 作者: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军) Adobe PDF(1388Kb)  |  收藏  |  浏览/下载:300/96  |  提交时间:2018/12/27 Combustion Condition Combustor Efficiency Improved Delayed Detached Eddy Simulations Initial Temperatures Laminar Flame Speed Scramjet Combustors Supersonic Combustion Turbulence-chemistry Interactions |
| Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文 APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253 作者: Li XP(李晓鹏); Zhou, Rui; Yao W(姚卫); Fan XJ(范学军); Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China. Adobe PDF(5723Kb)  |  收藏  |  浏览/下载:416/182  |  提交时间:2017/11/16 Underexpanded Jets Noncircular Jets Nozzle Geometry Large Eddy Simulation |
| 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) Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:440/216  |  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:258/87  |  提交时间:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |