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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：170/54  |  Submit date：2021/02/01
High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:  Yang L;  岳连捷;  张启帆;  张新宇
Adobe PDF(1289Kb)  |  Favorite  |  View/Download：233/60  |  Submit date：2021/01/12
Numerical simulation of acoustic scattering and flow-induced noise with sharp interface immersed boundary method 会议论文
AIAA Scitech 2020 Forum, Orlando, FL, 2020/1/6-10
Authors:  Zhao C;  Yang Y(杨焱);  Zhang T;  Dong HB
Adobe PDF(1785Kb)  |  Favorite  |  View/Download：143/56  |  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：291/152  |  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：183/79  |  Submit date：2021/06/11
Calculation method  Exhaust plume  Infrared spectroscopy  Radiation intensity  Three-dimensional space  
Airflow Inclination Sensor Based on Temperature Field 会议论文
3rd International Conference on Fluid Mechanics and Industrial Applications, Taiyuan, China, 2019-06-29~30
Authors:  Zheng YH;  Peng SL(彭世镠);  Xiao W
Adobe PDF(935Kb)  |  Favorite  |  View/Download：173/30  |  Submit date：2019/09/29
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：169/51  |  Submit date：2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
Supercritical GN2/GH2 jet modeled by the ECS method 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);  Jin YC(靳一超);  Lee YC(李亚超)
Adobe PDF(1048Kb)  |  Favorite  |  View/Download：183/72  |  Submit date：2020/11/20
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
Authors:  Chen L;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1280Kb)  |  Favorite  |  View/Download：190/77  |  Submit date：2020/11/20
Ventilated partial cavitating flow around a blunt body near the free surface 会议论文
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016, Honolulu, HI, United states, April 10, 2016 - April 15, 2016
Authors:  Wang YW(王一伟);  Wu XC(吴小翠);  Huang CG(黄晨光)
View  |  Adobe PDF(757Kb)  |  Favorite  |  View/Download：202/42  |  Submit date：2019/11/20
Axisymmetric bodies  Cavity boundaries  Free surfaces  High  speed underwater vehicles  Launching systems  Media properties  Unsteady behaviors  Ventilated cavitation