IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共8条,第1-8条 帮助

限定条件            
已选(0)清除 条数/页:   排序方式:
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  
Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1937Kb)  |  收藏  |  浏览/下载:262/86  |  提交时间:2018/10/30
Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration  
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  
长试验时间激波风洞测力技术研究 期刊论文
力学学报, 2016, 卷号: 48, 期号: 3, 页码: 545-556
作者:  汪运鹏;  刘云峰;  苑朝凯;  罗长童;  王春;  胡宗民;  韩桂来;  赵伟;  姜宗林
浏览  |  Adobe PDF(8800Kb)  |  收藏  |  浏览/下载:411/72  |  提交时间:2016/12/16
Shock Tunnel  Long-test Duration  Force Measurement  Strain-gaged Balance  
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2013, 卷号: 43, 页码: 46-52
作者:  Han GL(韩桂来);  Jiang ZL(姜宗林);  Han, GL (reprint author), Chinese Acad Sci, Stake Key Lab High Temp Gas Dynam LHD, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(548Kb)  |  收藏  |  浏览/下载:1097/326  |  提交时间:2013/05/31
Heat Conduction  Theoretical Investigation  Approximate Solution  Hypersonic  
支杆-钝头体带攻角流场和“军刺”挡板作用研究 期刊论文
力学学报, 2011, 卷号: 43, 期号: 5, 页码: 795-802
作者:  韩桂来;  姜宗林
Adobe PDF(1475Kb)  |  收藏  |  浏览/下载:718/146  |  提交时间:2012/04/01
支杆-钝头体  “军刺”挡板  带攻角飞行  三维数值模拟  
Conceptual Study on Non-ablative TPS for Hypersonic Vehicles 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
作者:  Jiang ZL(姜宗林);  Liu YF(刘云峰);  Han GL(韩桂来);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1058Kb)  |  收藏  |  浏览/下载:505/121  |  提交时间:2014/02/24
Experimental Demonstration Of A New Concept Of Drag Reduction And Thermal Protection For Hypersonic Vehicles 期刊论文
Acta Mechanica Sinica, 2009, 卷号: 25, 期号: 3, 页码: 417-419
作者:  Jiang ZL(姜宗林);  Liu YF(刘云峰);  Han GL(韩桂来);  Zhao W(赵威);  Jiang ZL
Adobe PDF(226Kb)  |  收藏  |  浏览/下载:884/207  |  提交时间:2009/08/03
Hypersonic Vehicle  Shock-reconstruction  Drag Reduction  Thermal Protection  Spike And Lateral Jets