|
Selected(0)Clear
Items/Page: Sort: |
| 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：301/154 | Submit date：2021/06/11 |
| A method for rapid generation of 3D infrared radiation intensity field of engine exhaust plume 会议论文
6th Symposium on Novel Optoelectronic Detection Technology and Applications, Beijing, PEOPLES R CHINA, 3 December 2019 through 5 December 2019
Authors: Bao XD(包醒东); Yu XL(余西龙); Wang Z.-H; Mao H.-X; Xiao Z.-H.
 Adobe PDF(602Kb) | Favorite | View/Download：191/81 | Submit date：2021/06/11
Calculation method Exhaust plume Infrared spectroscopy Radiation intensity Three-dimensional space |
| Spectral Radiant Intensity Calculation of Air in Shock Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Lyu, Jun Ming; Cheng, X. L.; Yu, J. J.; Li F(李飞); Yu XL(余西龙)
Adobe PDF(791Kb) | Favorite | View/Download：98/31 | Submit date：2023/03/17 |
| AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林); Teng HH(滕宏辉)
Adobe PDF(4139Kb) | Favorite | View/Download：319/71 | Submit date：2019/04/19 |
| 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)
Adobe PDF(1173Kb) | Favorite | View/Download：488/235 | 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 |
| A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Lee YC; Yao W(姚卫); Fan XJ(范学军); Yao, Wei(weiyao@imech.ac.cn)
Adobe PDF(1358Kb) | Favorite | View/Download：463/118 | Submit date：2018/01/16
Computational Fluid Dynamics Computer Software Digital Storage Kinetic Energy Kinetics Open Source Software Open Systems Runge Kutta Methods Shock Tubes Shock Waves Spacecraft Turbulence Two Phase Flow |
| 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)
Adobe PDF(623Kb) | Favorite | View/Download：305/108 | Submit date：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇)
Adobe PDF(517Kb) | Favorite | View/Download：354/115 | Submit date：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| 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
Authors: 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) | Favorite | View/Download：344/106 | Submit date：2018/01/16
Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Zeng W(曾徽); Lin X(林鑫); Zhen RP; Chen LZ; Li F(李飞); Yu XL(余西龙); Li, Fei(lifei@imech.ac.cn)
Adobe PDF(897Kb) | Favorite | View/Download：512/113 | Submit date：2018/01/16
Combustion Gas Absorption Infrared Devices Monopropellants Optical Parametric Oscillators Spacecraft |
