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| Numerical investigation on the performance of bluff body augmented micro cavity-combustor 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4932-4945 作者: Zhang Z; Wu K(吴坤); Yuen R; Yao W(姚卫); Wang J 浏览  |  Adobe PDF(3438Kb)  |  收藏  |  浏览/下载:311/109  |  提交时间:2020/04/07 Micro combustor Cavity Bluff body Combustion efficiency Local Damkohler number |
| 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:322/97  |  提交时间:2019/04/11 |
| 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 |
| Full-scale Improved Delayed Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 作者: Fan E; Wu K(吴坤); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(567Kb)  |  收藏  |  浏览/下载:333/100  |  提交时间: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 作者: Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(1783Kb)  |  收藏  |  浏览/下载:403/125  |  提交时间:2018/10/19 |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文 JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786 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(807Kb)  |  收藏  |  浏览/下载:338/105  |  提交时间:2018/07/17 |
| 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) Adobe PDF(805Kb)  |  收藏  |  浏览/下载:395/147  |  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) 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) 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 |
| Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文 53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017 作者: Fan E; Wu K(吴坤); Lee YC; Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(2297Kb)  |  收藏  |  浏览/下载:255/109  |  提交时间:2018/01/16 |