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| 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 |
| 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:260/144  |  提交时间:2021/06/11 |
| 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:140/43  |  提交时间:2020/11/20 Dynamic zone flamelet model GH2/GO2 Large Eddy Simulation (LES) Rocket combustor Turbulence-chemistry interaction |
| Influence of compressibility effect on supersonic combustion modeling 会议论文 AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019 作者: Chen L; Yao W(姚卫); Fan XJ(范学军) Adobe PDF(1280Kb)  |  收藏  |  浏览/下载:156/72  |  提交时间:2020/11/20 |
| A microscopic study of one-dimensional H2-O2 detonation using DSMC method 会议论文 31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018 作者: Yang C(杨超); Huang HJ(黄河激); Sun QH(孙泉华) Adobe PDF(936Kb)  |  收藏  |  浏览/下载:159/65  |  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:414/0  |  提交时间:2018/12/26 |
| 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:392/146  |  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: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) 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 |
| LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) Adobe PDF(1249Kb)  |  收藏  |  浏览/下载:300/89  |  提交时间:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |