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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
作者:  Zhao C;  Yang Y(杨焱);  Zhang T;  Dong HB
Adobe PDF(1785Kb)  |  收藏  |  浏览/下载：127/50  |  提交时间：2021/02/01
气相爆轰波DDT过程的物理模型 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
作者:  张文硕;  刘云峰;  姜宗林
浏览  |  Adobe PDF(1600Kb)  |  收藏  |  浏览/下载：267/75  |  提交时间：2019/11/21
气相爆轰  爆燃转爆轰  DDT  物理模型  
Experimental Research on the Detonation in Gaseous Mixtures with Suspended Aluminum Particles 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Zhang XY(张晓源);  Chen H(陈宏);  Li JP(李进平);  Zhang SZ(张仕忠);  Yu HR(俞鸿儒)
Adobe PDF(543Kb)  |  收藏  |  浏览/下载：38/19  |  提交时间：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
作者:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  收藏  |  浏览/下载：149/45  |  提交时间：2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
Aerodynamic Dispersion of Anode Arc Attachment Through a Converging-Diverging Nozzle 会议论文
18th Chinese National Conference on Plasma Science and Technology (CNCPST), Xian, PEOPLES R CHINA, JUL 26-29, 2017
作者:  Huang HJ(黄河激);  Pan WX(潘文霞);  Wu CK(吴承康)
浏览  |  Adobe PDF(891Kb)  |  收藏  |  浏览/下载：411/64  |  提交时间：2019/04/19
Aerodynamical dispersion  arc plasma generator  diffused arc root attachment  
A microscopic study of one-dimensional H2-O2 detonation using DSMC method 会议论文
31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018
作者:  Yang C(杨超);  Huang HJ(黄河激);  Sun QH(孙泉华)
Adobe PDF(936Kb)  |  收藏  |  浏览/下载：167/68  |  提交时间：2020/11/20
Full-scale Improved Delayed Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Fan E;  Wu K(吴坤);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(567Kb)  |  收藏  |  浏览/下载：337/101  |  提交时间：2018/12/26
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(805Kb)  |  收藏  |  浏览/下载：404/152  |  提交时间：2018/06/06
A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：285/113  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
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
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
Adobe PDF(1358Kb)  |  收藏  |  浏览/下载：431/110  |  提交时间：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