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Numerical studies of static aeroelastic effects on grid fin aerodynamic performances 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
作者:  Huang CD(黄程德);  Liu W(刘文);  Yang GW(杨国伟)
浏览  |  Adobe PDF(4021Kb)  |  收藏  |  浏览/下载：328/98  |  提交时间：2017/11/29
Aeroelasticity  Fluid-structure Interpolation  Grid Fin  Mesh Deformation  Radial Basis Function  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1654Kb)  |  收藏  |  浏览/下载：341/81  |  提交时间：2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
浏览  |  Adobe PDF(1315Kb)  |  收藏  |  浏览/下载：336/128  |  提交时间：2017/11/29
Molecular tagging velocimetry of NH fluorescence in a high-enthalpy rarefied gas flow 期刊论文
APPLIED PHYSICS B-LASERS AND OPTICS, 2017, 卷号: 123, 期号: 4
作者:  Zhang SH(张少华);  Yu XL(余西龙);  Yan H;  Huang HJ(黄河激);  Liu HL(刘宏立);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.;  Yu, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(1779Kb)  |  收藏  |  浏览/下载：358/127  |  提交时间：2017/07/24
Molecular Tagging Velocimetry  Nh Fluorescence  High-enthalpy  Rarefied Gas  
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：426/114  |  提交时间：2017/10/27
JF12长实验时间激波风洞10°尖锥气动力实验研究 期刊论文
气体物理, 2017, 卷号: 2, 期号: 02, 页码: 1-7
作者:  刘云峰;  汪运鹏;  苑朝凯;  罗长童;  姜宗林
浏览  |  Adobe PDF(2256Kb)  |  收藏  |  浏览/下载：312/56  |  提交时间：2017/12/22
Jf12长实验时间激波风洞  高超声速气动力特性  10°尖锥标模  真实气体效应  
高超声速飞行目标尾焰红外辐射测量 期刊论文
气体物理, 2017, 卷号: 2, 期号: 02, 页码: 47-53
作者:  刘立拓;  余西龙;  陈宏;  张仕忠;  张晓源
浏览  |  Adobe PDF(1667Kb)  |  收藏  |  浏览/下载：322/100  |  提交时间：2017/12/22
高超声速飞行器  尾焰  红外辐射  
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：277/112  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
Surrogate Based Optimization of Aerodynamic Noise for Streamlined Shape of High Speed Trains 期刊论文
APPLIED SCIENCES-BASEL, 2017, 卷号: 7, 期号: 2
作者:  Sun ZX(孙振旭);  Zhang Y;  Yang GW(杨国伟);  Sun, ZX (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(6165Kb)  |  收藏  |  浏览/下载：612/325  |  提交时间：2017/07/24
Aerodynamic Noise  Nlas  Kriging Model  Cross Validation  Equivalent Continuous Spl  
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：422/107  |  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