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激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:  王粤;  汪运鹏;  姜宗林
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两级入轨  轨迹捕获  激波风洞  多体分离  动态试验  试验技术  
鼓包诱导斜爆震波的数值研究 期刊论文
推进技术, 2022, 卷号: 43, 期号: 05, 页码: 190-201
Authors:  韩信;  张文硕;  张子健;  刘云峰;  姜宗林
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斜爆震发动机  鼓包  加速起爆  来流扰动  流动控制  
高超声速高焓条件下的内嵌式温敏漆测量方法 期刊论文
力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58
Authors:  苑朝凯;  姜宗林
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温敏漆  热流密度场  辐射效应  高超声速流动  辨识方法  
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  
超常环境力学领域研究新进展—–《力学学报》极端力学专题研讨会综述报告 期刊论文
力学学报, 2021, 卷号: 53, 期号: 02, 页码: 589-599
Authors:  姜宗林;  刘俊丽;  苑朝凯;  陈海璇;  陆夕云
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极端力学  力学学报  超常环境力学领域  研究进展  研究展望  
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  
高超声速喷管设计理论与方法 期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors:  汪运鹏;  姜宗林
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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