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基于激波管评价的单兵头面部装备冲击波防护性能研究 期刊论文
爆炸与冲击, 2021, 卷号: 41, 期号: 08, 页码: 179-191
作者:  康越;  张仕忠;  张远平;  柳占立;  黄献聪;  马天
Adobe PDF(8211Kb)  |  收藏  |  浏览/下载：264/31  |  提交时间：2021/11/12
爆炸冲击波  冲击波防护  单兵装备  激波管  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载：322/169  |  提交时间：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
页岩气开采中的若干力学前沿问题 期刊论文
力学进展, 2019, 卷号: 49, 期号: 00, 页码: 1-236
作者:  刘曰武;  高大鹏;  李奇;  万义钊;  段文杰;  曾霞光;  李明耀;  苏业旺;  范永波;  李世海;  鲁晓兵;  周东;  陈伟民;  傅一钦;  姜春晖;  侯绍继;  潘利生;  魏小林;  胡志明;  端祥刚;  高树生;  沈瑞;  常进;  李晓雁;  柳占立;  魏宇杰;  郑哲敏
Adobe PDF(109408Kb)  |  收藏  |  浏览/下载：302/39  |  提交时间：2019/09/12
页岩气  压裂  力学性质  数值模拟  监测技术  渗流  
An efficient unstructured WENO method for supersonic reactive flows 期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
作者:  Zhao WG;  Zheng HW(郑洪伟);  Liu FJ;  Shi XT;  Gao J;  Hu N;  Lv M;  Chen SC;  Zhao HD
浏览  |  Adobe PDF(3673Kb)  |  收藏  |  浏览/下载：379/94  |  提交时间：2018/10/30
Supersonic reactive flows  Adaptive splitting scheme  Unstructured grids  WENO reconstruction  
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：458/107  |  提交时间：2017/12/18
Hypersonic  Aerodynamic Measurement  Theoretical Study  Vibration  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
作者:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1080Kb)  |  收藏  |  浏览/下载：512/126  |  提交时间：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
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：337/129  |  提交时间：2017/11/29
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1162Kb)  |  收藏  |  浏览/下载：329/81  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
作者:  Zhong FQ(仲峰泉);  Ma SG;  Zhang XY(张新宇);  Sung CJ;  Niemeyer KE;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1318Kb)  |  收藏  |  浏览/下载：291/93  |  提交时间：2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time