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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：147/43 | 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：364/129 | Submit date：2020/08/27
Artificial Neural Network (Ann) Principle Of Extended Corresponding State (Ecs) Rp-3 Kerosene Superitical Pressure Openfoam |
| 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
Authors: Li B(李波); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(1358Kb) | Favorite | View/Download：177/59 | Submit date：2021/02/01 |
| Flow Modulation and Mixing Enhancement of Highly Underexpanded Jet by Vortex Excitation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2462-2474
Authors: Wang Y(汪也); Wu K(吴坤); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(6305Kb) | Favorite | View/Download：377/96 | Submit date：2020/07/06 |
| Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
Authors: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军)
View | Adobe PDF(1820Kb) | Favorite | View/Download：489/162 | Submit date：2018/12/27
Supersonic combustion Flame stabilization mode DLR Strut injection scheme Stagnation Temperature Overall equivalence ratio |
| 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
Authors: Yao W(姚卫); Wu K(吴坤); Lee YC(李亚超); Fan XJ(范学军)
 Adobe PDF(1156Kb) | Favorite | View/Download：460/0 | Submit date：2018/12/26 |
| Low-Dissipative Hybrid Compressible Solver Designed for Large-Eddy Simulation of Supersonic Turbulent Flows 期刊论文
AIAA JOURNAL, 2018, 卷号: 56, 期号: 8, 页码: 3086-3096
Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军)
View | Adobe PDF(1783Kb) | Favorite | View/Download：430/130 | Submit date：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
Authors: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军)
View | Adobe PDF(1388Kb) | Favorite | View/Download：341/113 | Submit date：2018/12/27
Combustion Condition Combustor Efficiency Improved Delayed Detached Eddy Simulations Initial Temperatures Laminar Flame Speed Scramjet Combustors Supersonic Combustion Turbulence-chemistry Interactions |
| 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
Authors: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军)
View | Adobe PDF(1377Kb) | Favorite | View/Download：313/120 | Submit date：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems |
| 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：485/234 | 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 |
