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Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
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Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:  Peng, Di;  Liu, Xu;  Jiao, Lingrui;  Li, Ziyan;  Wen, Xin;  Yuan CK(苑朝凯);  Han GL(韩桂来);  Liu YF(刘云峰);  Liu, Yingzheng;  Jiang ZL(姜宗林)
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Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation  
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  Favorite  |  View/Download：437/79  |  Submit date：2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
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：363/179  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(1551Kb)  |  Favorite  |  View/Download：291/88  |  Submit date：2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  Favorite  |  View/Download：288/102  |  Submit date：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40
Authors:  Zhang ZJ(张子健);  Wen CY;  Liu YF(刘云峰);  Zhang DL(张德良);  Jiang ZL(姜宗林)
View  |  Adobe PDF(4374Kb)  |  Favorite  |  View/Download：443/154  |  Submit date：2019/09/09
Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation  
Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1468Kb)  |  Favorite  |  View/Download：375/113  |  Submit date：2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel  
Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile 期刊论文
SHOCK WAVES, 2017, 卷号: 27, 期号: 5, 页码: 771-779
Authors:  Li, X. D.;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Hu, ZM (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View  |  Adobe PDF(2166Kb)  |  Favorite  |  View/Download：453/115  |  Submit date：2017/11/16
Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1080Kb)  |  Favorite  |  View/Download：538/136  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel