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Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
Authors:  Yao KP(姚克鹏);  Yang PF(杨鹏飞);  Wang C(王春);  Jiang ZL(姜宗林)
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Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
Authors:  Nie SJ(聂少军);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Convolutional neural net-works  Deep learning  Frequency domain analysis  Force measurement  Time domain analysis  Recurrent neural networks  
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:  Zhang, Zijian;  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Chemical equilibrium  Detonation  Dissociated air  Shock relation  Theoretical solution  
An experimental study of formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2022, 卷号: 237, 页码: 5
Authors:  Zhang ZJ(张子健);  Wen, Chihyung;  Yuan CK(苑朝凯);  Liu YF(刘云峰);  Han GL(韩桂来);  Wang C(王春);  Jiang ZL(姜宗林)
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Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects  
Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu, Yunfeng;  Wang, Chun
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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)
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Hypersonics  Shock tunnels  Flow characteristics  
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:  Zhang ZJ(张子健);  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3599Kb)  |  Favorite  |  View/Download：354/90  |  Submit date：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation