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| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文 Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995 Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9707Kb)  |  Favorite  |  View/Download:334/97  |  Submit date:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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:168/53  |  Submit date:2021/02/01 |
| Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文 INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696 Authors: Xue R(薛瑞); Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C Adobe PDF(3251Kb)  |  Favorite  |  View/Download:371/113  |  Submit date:2020/07/06 Compressible boundary layer combustion Skin-friction reduction Shock train/flame interaction |
| Magnetic Actuation of Flexible Microelectrode Arrays for Neural Activity Recordings 期刊论文 NANO LETTERS, 2019, 卷号: 19, 期号: 11, 页码: 8032-8039 Authors: Gao L; Wang JF; Guan SL; Du MD; Wu K(吴坤); Xu K; Zou L; Tian HH; Fang Y View  |  Adobe PDF(7003Kb)  |  Favorite  |  View/Download:395/199  |  Submit date:2020/03/11 flexible microelectrode magnetic actuation nanoscale roughness neural recording inflammatory response |
| Effect of pressure on joint cascade of kinetic energy and helicity in compressible helical turbulence 期刊论文 PHYSICAL REVIEW E, 2019, 卷号: 99, 期号: 3, 页码: 11 Authors: Yan Z(闫政); Li XL(李新亮); Wang JC(汪建春); Yu CP(于长平) View  |  Adobe PDF(6549Kb)  |  Favorite  |  View/Download:334/108  |  Submit date:2019/05/29 |
| 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 |
| 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:167/50  |  Submit date:2020/11/20 Dynamic zone flamelet model GH2/GO2 Large Eddy Simulation (LES) Rocket combustor Turbulence-chemistry interaction |
| 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:476/230  |  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) View  |  Adobe PDF(623Kb)  |  Favorite  |  View/Download:280/97  |  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) View  |  Adobe PDF(832Kb)  |  Favorite  |  View/Download:307/93  |  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 |