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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 Authors: Li B(李波); Yao W(姚卫); Li YC(李亚超); Fan XJ(范学军) Adobe PDF(5169Kb)  |  Favorite  |  View/Download:141/40  |  Submit date:2022/10/25 Heat release rate (HRR) Artificial neural network (ANN) Proper orthogonal -12omposition (POD) Chemiluminescence Supersonic hydrogen flame |
| Development and application of ANN model for property prediction of supercritical kerosene 期刊论文 Computers and Fluids, 2020, 卷号: 209, 期号: 2020, 页码: 1-18 Authors: Li B(李波); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(10546Kb)  |  Favorite  |  View/Download:359/127  |  Submit date:2020/08/27 Artificial Neural Network (Ann) Principle Of Extended Corresponding State (Ecs) Rp-3 Kerosene Superitical Pressure Openfoam |
| 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 Authors: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军) Adobe PDF(862Kb)  |  Favorite  |  View/Download:346/102  |  Submit date:2019/04/11 |
| 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 Authors: Li B; Lee YC(李亚超); Yao W(姚卫); Lu Y(陆阳); Fan XJ(范学军) View  |  Adobe PDF(1813Kb)  |  Favorite  |  View/Download:333/87  |  Submit date: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 Authors: Li B(李波); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1813Kb)  |  Favorite  |  View/Download:242/72  |  Submit date:2020/08/27 |
| 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 Authors: 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) View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download:479/232  |  Submit date: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 Authors: Yao W(姚卫); Fan XJ(范学军) Adobe PDF(623Kb)  |  Favorite  |  View/Download:285/99  |  Submit date:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| 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 Authors: Yao W(姚卫); Fan XJ(范学军) Adobe PDF(832Kb)  |  Favorite  |  View/Download:309/94  |  Submit date: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 |