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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
Authors:  Teng, Honghui;  Zhang, Yuhang;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
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Double wedge  Hypersonic flow  Initiation structures  Oblique detonation  Shock interactions  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
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Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
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)
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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)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
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)
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hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
An efficient unstructured WENO method for supersonic reactive flows 期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
Authors:  Zhao WG;  Zheng HW(郑洪伟);  Liu FJ;  Shi XT;  Gao J;  Hu N;  Lv M;  Chen SC;  Zhao HD
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Supersonic reactive flows  Adaptive splitting scheme  Unstructured grids  WENO reconstruction  
Theoretical analysis on deflagration-to-detonation transition 期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 8, 页码: 84703
Authors:  Liu YF(刘云峰);  Shen H(沈还);  Zhang DL(张德良);  Jiang ZL(姜宗林)
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deflagration  detonation  deflagration-to-detonation transition  
Theoretical approach to one-dimensional detonation instability 期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2016, 卷号: 37, 期号: 9, 页码: 1231-1238
Authors:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(514Kb)  |  Favorite  |  View/Download:480/97  |  Submit date:2016/12/08
Detonation Wave  Detonation Instability  Shock Wave  Chemical Reaction