IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共6条,第1-6条 帮助

限定条件                
已选(0)清除 条数/页:   排序方式:
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  
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
作者:  Yuan CK(苑朝凯);  Zhou K(周凯);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1471Kb)  |  收藏  |  浏览/下载:232/57  |  提交时间:2020/07/06
Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
作者:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1468Kb)  |  收藏  |  浏览/下载:327/94  |  提交时间:2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel  
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:334/91  |  提交时间:2017/09/19
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:351/98  |  提交时间:2016/06/28
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