IMECH-IR

浏览/检索结果: 共52条,第1-10条 帮助

限定条件    
已选(0)清除 条数/页:   排序方式:
Hypervelocity Test with a Detonation-Driven Expansion Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭峻);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(297Kb)  |  收藏  |  浏览/下载:183/64  |  提交时间:2020/01/06
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:338/63  |  提交时间:2020/01/06
High-Enthalpy Flow Investigations by UV Laser-Induced Fluorescence 会议论文
2019 PhotonIcs and Electromagnetics Research Symposium - Spring, PIERS-Spring 2019, Rome, Italy, June 17, 2019 - June 20, 2019
作者:  Yan H(严浩);  Zhang SH(张少华);  Wang FY(王方仪);  Yu XL(余西龙)
Adobe PDF(315Kb)  |  收藏  |  浏览/下载:332/73  |  提交时间:2020/11/20
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:155/71  |  提交时间:2020/11/20
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1120Kb)  |  收藏  |  浏览/下载:485/103  |  提交时间:2018/12/26
A hybrid kinetic WENO scheme for compressible flow simulations 会议论文
The 10th International Conference on Computational Fluid Dynamics (ICCFD10), Barcelona,Spain, July 9-13, 2018
作者:  Liu HW(刘洪伟);  Yu ZP(于长平);  Li XL(李新亮)
浏览  |  Adobe PDF(878Kb)  |  收藏  |  浏览/下载:388/75  |  提交时间:2018/11/09
Gas Kinetic Theory  Numerical Dissipation  Weno Method  Hybrid Numerical Flux  High Order Schemes  
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:389/145  |  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:209/63  |  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:276/112  |  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:438/216  |  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