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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
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：357/178  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Continuum perspective of bulk viscosity in compressible fluids 期刊论文
JOURNAL OF FLUID MECHANICS, 2017, 卷号: 812, 页码: 966-990
Authors:  Li XD;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(4637Kb)  |  Favorite  |  View/Download：473/154  |  Submit date：2017/04/26
On the numerical technique for the simulation of hypervelocity test flows 期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
Authors:  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林);  Khoo BC;  Hu ZM(胡宗民)
View  |  Adobe PDF(1617Kb)  |  Favorite  |  View/Download：1605/930  |  Submit date：2014/11/27
Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
A New Flux Splitting Scheme for Euler Equations of Gas Dynamics 会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
Authors:  Li XD(李馨东);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1140Kb)  |  Favorite  |  View/Download：482/170  |  Submit date：2015/09/29
Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme  
Numerical simulation of deflagration to detonation transition in a straight duct: Effects of energy release and detonation stability 期刊论文
Advances in Applied Mathematics and Mechanics, 2014, 卷号: 6, 期号: 6, 页码: 718-731
Authors:  Dou HS;  Hu ZM(胡宗民);  Khoo BC;  Jiang ZL(姜宗林)
View  |  Adobe PDF(487Kb)  |  Favorite  |  View/Download：841/258  |  Submit date：2014/11/27
Numerical Simulation  Detonation  Ddt  Energy Release  Duct