IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Selected(0)Clear Items/Page:    Sort:
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106./通讯作者:Lin, MY (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China., Lin, MY (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Authors:  Peng J(彭俊);  Li S(李帅);  Yang F(杨帆);  Lin MY(林明月);  Han GL(韩桂来);  Hu ZM(胡宗民)
Adobe PDF(2838Kb)  |  Favorite  |  View/Download:82/11  |  Submit date:2023/04/20
Shock interactions  Transitional configuration  Aerodynamic heating  Shear layer  Mach interaction  
Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184./通讯作者:Yang, Pengfei
Authors:  Teng, Honghui;  Zhang, Yuhang;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(1747Kb)  |  Favorite  |  View/Download:253/52  |  Submit date:2022/07/18
Double wedge  Hypersonic flow  Initiation structures  Oblique detonation  Shock interactions  
Thermochemical non-equilibrium effects on hypersonic shock wave/turbulent boundary-layer interaction 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 192, 页码: 1-14./通讯作者:Liu, Jun
Authors:  Jiang, Hao;  Liu, Jun;  Luo, Shichao;  Huang, Wei;  Wang, Junyuan;  Liu MK(刘美宽)
Adobe PDF(9113Kb)  |  Favorite  |  View/Download:327/61  |  Submit date:2022/05/17
Hypersonic flow  Shock wave/turbulent boundary-layer interactions  Thermochemical non-equilibrium  Turbulence model  
Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme 期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118./通讯作者:Sun, Q.
Authors:  Chen S;  Sun QH(孙泉华);  Klioutchnikov I;  Olivier H
View  |  Adobe PDF(1365Kb)  |  Favorite  |  View/Download:403/152  |  Submit date:2019/06/10
Shock wave/boundary-layer interactions  Real gas effects  Chemical nonequilibrium  High-order scheme  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
View  |  Adobe PDF(2110Kb)  |  Favorite  |  View/Download:433/150  |  Submit date:2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download:449/115  |  Submit date:2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows