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Numerical study of oblique detonation initiations with chain-branching kinetics 会议论文
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, 9-13 January 2017
作者:  Teng HH(滕宏辉);  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(464Kb)  |  收藏  |  浏览/下载：276/109  |  提交时间：2018/01/16
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  
One-Step Direct Aeroacoustic Simulation Using Space-Time Conservation Element and Solution Element Method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Ho CY;  Leung RCK;  Zhou K;  Lam GCY;  Jiang ZL(姜宗林)
Adobe PDF(400Kb)  |  收藏  |  浏览/下载：494/200  |  提交时间：2014/01/14
Aeroacoustics  Caa  Ce/se Method  Acoustic Wave  Supersonic Jet  
Research progress on high-enthalpy and hypersonic flows 会议论文
5th International Conference on Fluid Mechanics, Shanghai, PEOPLES R CHINA, AUG 15-19, 2007
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Lin ZB(林贞彬);  Jiang Z
Adobe PDF(690Kb)  |  收藏  |  浏览/下载：877/240  |  提交时间：2009/07/23
Hypersonic Flows  Detonation Driver  Shock-reflected Tunnels  Shock-expanded Tube  Heat Transfer