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Aerodynamic measurement of a large aircraft model in hypersonic flow 期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Zhang DL(张德良);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(4916Kb)  |  收藏  |  浏览/下载：457/106  |  提交时间：2017/12/18
Hypersonic  Aerodynamic Measurement  Theoretical Study  Vibration  
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：424/107  |  提交时间：2017/11/16
Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration  
Initiation structure of oblique detonation waves behind conical shocks 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
作者:  Yang PF(杨鹏飞);  Ng, Hoi Dick;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
浏览  |  Adobe PDF(5788Kb)  |  收藏  |  浏览/下载：449/99  |  提交时间：2017/11/16
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
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
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(6096Kb)  |  收藏  |  浏览/下载：306/87  |  提交时间：2018/01/16
圆球诱发斜爆轰波的数值研究 期刊论文
力学学报, 2017, 卷号: 49, 期号: 02, 页码: 268-273
作者:  方宜申;  胡宗民;  滕宏辉;  姜宗林
浏览  |  Adobe PDF(489Kb)  |  收藏  |  浏览/下载：311/75  |  提交时间：2017/12/22
斜爆轰  氢氧  起爆  熄爆  
Initiation characteristics of wedge-induced oblique detonation waves in a stoichiometric hydrogen-air mixture 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2735-2742
作者:  Teng HH(滕宏辉);  Ng HD;  Jiang ZL(姜宗林);  Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1409Kb)  |  收藏  |  浏览/下载：330/119  |  提交时间：2017/07/24
Oblique Detonation  Formation Structure  Hydrogen  Shock Wave  Detailed Chemistry  
Elite bases regression: A real-time algorithm for symbolic regression 会议论文
13th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery, ICNC-FSKD 2017, Guilin, Guangxi, China, July 29, 2017 - July 31, 2017
作者:  Chen C(陈辰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(245Kb)  |  收藏  |  浏览/下载：210/50  |  提交时间：2018/11/08
Data mining  Fuzzy systems  Genetic algorithms  Genetic programming  Iterative methods  Learning systems  Comparative studies  Correlation coefficient  Function extraction  Large  scale problem  Machine learning methods  Real time algorithms  Symbolic regression  Symbolic regression problems  
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载：386/68  |  提交时间：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis