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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 Authors: Li B(李波); Yao W(姚卫); Fan XJ(范学军) Adobe PDF(1358Kb)  |  Favorite  |  View/Download:158/49  |  Submit date: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 Authors: Yao W(姚卫); Chen L(陈留) Adobe PDF(2272Kb)  |  Favorite  |  View/Download:277/149  |  Submit date: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 Authors: Yao W(姚卫); Li B(李波) Adobe PDF(1665Kb)  |  Favorite  |  View/Download:158/49  |  Submit date:2020/11/20 Dynamic zone flamelet model GH2/GO2 Large Eddy Simulation (LES) Rocket combustor Turbulence-chemistry interaction |
| 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:425/0  |  Submit date:2018/12/26 |
| Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 Authors: Wang Y; Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(1120Kb)  |  Favorite  |  View/Download:502/109  |  Submit date:2018/12/26 |
| Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015 Authors: Yao W(姚卫); Wang J(王晶); Lu Y(陆阳); Li XP(李晓鹏); Fan XJ(范学军) Adobe PDF(1195Kb)  |  Favorite  |  View/Download:488/176  |  Submit date:2016/07/01 Adiabatic Flame Temperature Combustion Directed Graphs Flow Separation Heat Flux Kerosene Large Eddy Simulation Musculoskeletal System Real Time Systems Sensitivity Analysis Spacecraft Transients |