IMECH-IR

浏览/检索结果: 共41条,第1-10条 帮助

限定条件                    
已选(0)清除 条数/页:   排序方式:
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
作者:  Yang L;  岳连捷;  张启帆;  张新宇
Adobe PDF(1289Kb)  |  收藏  |  浏览/下载:203/49  |  提交时间:2021/01/12
Analysis of the influence of the vane width on the fluid transmission performance in the vane-type tank 会议论文
International Conference on Energy, Power and Mechanical Engineering (EPME2019), Guangzhou, China, 20-22 December 2019
作者:  Zhuang BT(庄宝唐);  Li Y;  Pan HL;  Rui W
浏览  |  Adobe PDF(499Kb)  |  收藏  |  浏览/下载:207/57  |  提交时间:2020/06/15
The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Li XD(李旭东);  Shi CM(师曾敏)
浏览  |  Adobe PDF(376Kb)  |  收藏  |  浏览/下载:340/63  |  提交时间:2020/01/06
Investigation of shock attenuation in a shock tube 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:  Xue XW(薛晓薇);  Chen S;  Sun QH(孙泉华)
Adobe PDF(1688Kb)  |  收藏  |  浏览/下载:157/72  |  提交时间:2020/11/20
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)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载:395/147  |  提交时间:2018/06/06
THE MECHANISM OF THREE-DIMENSION STEADY SHOCK WAVE INTERACTION 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者:  Wang C(王春);  Yang RX(杨瑞欣);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(3021Kb)  |  收藏  |  浏览/下载:214/65  |  提交时间:2019/04/19
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)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载:280/113  |  提交时间:2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
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
作者:  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)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:441/217  |  提交时间: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
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
浏览  |  Adobe PDF(1358Kb)  |  收藏  |  浏览/下载:424/107  |  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  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(566Kb)  |  收藏  |  浏览/下载:329/72  |  提交时间:2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels