IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共11条,第1-10条 帮助

限定条件            
已选(0)清除 条数/页:   排序方式:
斜爆轰发动机燃烧机理试验研究 期刊论文
推进技术, 2021, 卷号: 42, 期号: 04, 页码: 786-794
作者:  张子健;  韩信;  马凯夫;  张文硕;  刘云峰;  苑朝凯;  姜宗林
Adobe PDF(6817Kb)  |  收藏  |  浏览/下载:249/65  |  提交时间:2021/04/19
斜爆轰发动机  超声速燃烧  激波诱导燃烧  斜爆轰波  斜激波  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:252/101  |  提交时间:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
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  
振动激发对高超声速气动力/热影响 期刊论文
力学学报, 2017, 卷号: 49, 期号: 03, 页码: 616-626
作者:  张子健;  刘云峰;  姜宗林
浏览  |  Adobe PDF(711Kb)  |  收藏  |  浏览/下载:365/74  |  提交时间:2017/12/22
振动激发  气动力/热  边界层  高温气体效应  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(764Kb)  |  收藏  |  浏览/下载:335/91  |  提交时间:2017/09/19
Force measurement using strain-gauge balance in a shock tunnel with long test duration 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2016, 卷号: 87, 期号: 5, 页码: 55108
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(6592Kb)  |  收藏  |  浏览/下载:319/89  |  提交时间:2016/09/14
Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
作者:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(764Kb)  |  收藏  |  浏览/下载:353/99  |  提交时间:2016/06/28
Force measurement in a shock tunnel with 100 milliseconds test duration 会议论文
34th AIAA Applied Aerodynamics Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
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(6592Kb)  |  收藏  |  浏览/下载:307/78  |  提交时间:2017/05/05
Aerodynamic Forces  Chinese Academy Of Sciences  Different Structure  Digital Filtering  Large  Scale Modeling  Low  Frequency Vibration  Strain Gauge Balances  Strain Gauge Sensors  
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  
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(5104Kb)  |  收藏  |  浏览/下载:239/45  |  提交时间:2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow