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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：351/177  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
On the ideal weights for WENO/WENO-like finite difference schemes for the first derivative, I 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 卷号: 31, 期号: 7, 页码: 12
Authors:  Kang J(康健);  Li XL(李新亮)
Adobe PDF(584Kb)  |  Favorite  |  View/Download：189/51  |  Submit date：2020/09/07
Finite difference  weighted essentially non-oscillatory  ideal weights  proof  
Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner 期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
Authors:  Tong FL(童福林);  Li XL(李新亮);  Yuan XX;  Yu ZP(于长平)
View  |  Adobe PDF(7909Kb)  |  Favorite  |  View/Download：374/120  |  Submit date：2020/04/07
Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner