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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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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)
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View/Download:89/0
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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)
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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)
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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.
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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.
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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.
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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)
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Submit date:2015/09/14
Shock Wave
Boundary Layer
Aerodynamic Heating