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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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Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
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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)
Adobe PDF(6382Kb)  |  Favorite  |  View/Download:229/34  |  Submit date:2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
一维与二维爆轰传播的时空关联特性数值研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 07, 页码: 2069-2078
Authors:  张文硕;  杨鹏飞;  姜宗林;  刘云峰
Adobe PDF(1701Kb)  |  Favorite  |  View/Download:216/51  |  Submit date:2021/08/25
斜爆轰  活塞  时空关联  基元反应模型  
激波风洞高低压段钢膜片破裂特性研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1747-1757
Authors:  聂少军;  汪运鹏;  薛晓鹏;  姜宗林
Adobe PDF(7665Kb)  |  Favorite  |  View/Download:258/67  |  Submit date:2021/11/12
激波风洞  主膜片  爆轰驱动  破裂特性  数值模拟  
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed (vol 43, pg 46, 2013) 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2021, 卷号: 124, 页码: 1
Authors:  Han GL(韩桂来);  Qi L(齐力);  Jiang ZL(姜宗林)
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JF-12激波风洞在火星进入环境下的运行特性 期刊论文
航空学报, 2021, 卷号: 42, 期号: 03, 页码: 189-200
Authors:  韩子健;  彭俊;  胡宗民;  韩桂来;  姜宗林
Adobe PDF(5070Kb)  |  Favorite  |  View/Download:355/88  |  Submit date:2021/04/19
火星探测  反向爆轰驱动激波风洞  二氧化碳  缝合运行状态  驻室压力  
关于超声速燃烧与高超动力 期刊论文
力学进展, 2021, 卷号: 51, 期号: 01, 页码: 130-140
Authors:  姜宗林
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超燃冲压发动机  临界参数  超声速燃烧  驻定斜爆轰冲压发动机  斜爆轰  
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)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download:286/58  |  Submit date:2021/05/17
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)
Adobe PDF(3477Kb)  |  Favorite  |  View/Download:269/53  |  Submit date:2021/03/30
Temperature-sensitive paint  Time-resolved measurement  Hypersonic flow  Background radiation