IMECH-IR

Browse/Search Results:  1-10 of 63 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  Favorite  |  View/Download:180/49  |  Submit date:2022/07/04
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
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:141/54  |  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:288/151  |  Submit date:2021/06/11
Application of NO Laser-Induced Fluorescence in JF-10 Detonation-Driven Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Yan H(严浩);  Zhang SH(张少华);  Yu XL(余西龙)
Adobe PDF(374Kb)  |  Favorite  |  View/Download:92/31  |  Submit date:2023/03/17
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  
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:179/70  |  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:188/76  |  Submit date:2020/11/20
A novel method of cooling channel optimization for active-cooled structure using the calculus of variations 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Li X(李轩);  Lu Y(陆阳);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(705Kb)  |  Favorite  |  View/Download:190/66  |  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:198/40  |  Submit date:2019/11/20
Axisymmetric bodies  Cavity boundaries  Free surfaces  High  speed underwater vehicles  Launching systems  Media properties  Unsteady behaviors  Ventilated cavitation