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Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile 期刊论文
SHOCK WAVES, 2017, 卷号: 27, 期号: 5, 页码: 771-779
作者:  Li, X. D.;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Hu, ZM (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(2166Kb)  |  收藏  |  浏览/下载：419/107  |  提交时间：2017/11/16
Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration  
High-Pressure Capturing Wing Configurations 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
作者:  Cui K(崔凯);  Li GL;  Xiao Y(肖尧);  Xu YZ;  Cui,K(reprint author), Chinese Acad Sci, Inst Mech
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载：611/169  |  提交时间：2017/07/24
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(419Kb)  |  收藏  |  浏览/下载：425/114  |  提交时间：2017/10/27
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：275/112  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
作者:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1329Kb)  |  收藏  |  浏览/下载：562/112  |  提交时间：2017/03/28
Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity  
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：434/214  |  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：416/104  |  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  
Development of zone flamelet model for scramjet combustor modeling 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);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：250/83  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
可压缩流动中间断问题的高分辨率数值求解方法及应用 学位论文
博士论文，北京: 中国科学院大学, 2017
作者:  刘利
Adobe PDF(16708Kb)  |  收藏  |  浏览/下载：351/12  |  提交时间：2019/05/15
高压捕获翼新型气动构型研究 学位论文
博士论文，北京: 中国科学院大学, 2017
作者:  李广利
Adobe PDF(12704Kb)  |  收藏  |  浏览/下载：980/46  |  提交时间：2017/07/07