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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:340/173  |  Submit date:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
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:1582/920  |  Submit date:2014/11/27
Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
Analysis of the test condition of a shock-expansion tube: JF-16 会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012-10
Authors:  Hu ZM(胡宗民);  Wu B(吴波);  Jiang ZL(姜宗林)
Adobe PDF(264Kb)  |  Favorite  |  View/Download:845/248  |  Submit date:2013/03/16
Shock-expansion Tube  Computation  Spurious Oscillation  Flus Splliting  
JF16 膨胀管运行条件分析的数值问题 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:  胡宗民;  李进平;  姜宗林
Adobe PDF(909Kb)  |  Favorite  |  View/Download:487/153  |  Submit date:2014/01/23
高焓  膨胀管  爆轰驱动  接触间断  数值振荡