IMECH-IR

Browse/Search Results:  1-7 of 7 Help

Selected(0)Clear Items/Page:    Sort:
Experimental Study on Aerodynamic Heating of Hypersonic Boundary-Layer Blowing 期刊论文
AIAA JOURNAL, 2024, 页码: 6./通讯作者:Han, Guilai
Authors:  Li ZX(李宗贤);  Liu MK(刘美宽);  Han GL(韩桂来);  Wang DG(王大高);  Jiang ZL(姜宗林)
Favorite  |  View/Download:89/0  |  Submit date:2024/10/08
Heat Flux Distribution  Adverse Pressure Gradient  Aerodynamic Heating  Hypersonic Boundary Layer  Wind Tunnel Tests  Boundary Layer Control  
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:86/11  |  Submit date:2023/04/20
Shock interactions  Transitional configuration  Aerodynamic heating  Shear layer  Mach interaction  
Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8./通讯作者:Li, J. P.
Authors:  Wang Q(汪球);  Li JP(李进平);  Luo K(罗凯);  Li JW(栗继伟);  Zhao W(赵伟)
Adobe PDF(1158Kb)  |  Favorite  |  View/Download:395/91  |  Submit date:2021/05/17
Hypersonic  Aerodynamic heating  Detached bow shock  Shock tube  expansion tube  
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
Authors:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(763Kb)  |  Favorite  |  View/Download:666/270  |  Submit date:2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 7, 页码: 1120-1129
Authors:  Li, XD;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(2496Kb)  |  Favorite  |  View/Download:422/138  |  Submit date:2016/09/14
Hypersonic Flow  Aerodynamic Heating  Thermal Protection System  Forward-facing Cavity  
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(860Kb)  |  Favorite  |  View/Download:506/220  |  Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER 期刊论文
Acta Mechanica Sinica, 1992, 卷号: 8, 期号: 3, 页码: 224-230
Authors:  Tang GM(唐贵明);  Yu HR(俞鸿儒)
View  |  Adobe PDF(663Kb)  |  Favorite  |  View/Download:275/130  |  Submit date:2015/09/14
Shock Wave  Boundary Layer  Aerodynamic Heating