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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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微重力重点实验室 [1]
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姜宗林 [20]
刘云峰 [8]
滕宏辉 [8]
李进平 [5]
胡宗民 [5]
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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
Adobe PDF(3358Kb)
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View/Download:240/66
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Submit date:2022/06/10
斜爆震发动机
鼓包
加速起爆
来流扰动
流动控制
气相爆轰驱动二级轻气炮内弹道数值模拟
期刊论文
力学学报, 2022, 卷号: 54, 期号: 03, 页码: 810-821
Authors:
尚甲豪
;
邢好运
;
汪球
;
李进平
;
赵伟
;
魏炳忱
Adobe PDF(3263Kb)
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View/Download:298/65
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Submit date:2022/06/10
爆轰驱动
轻气炮
数值模拟
发射性能
内弹道
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)
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View/Download:238/36
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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)
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View/Download:221/54
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Submit date:2021/08/25
斜爆轰
活塞
时空关联
基元反应模型
斜爆轰波系在受限空间内的演变及其临界条件的数值研究
期刊论文
推进技术, 2021, 卷号: 42, 期号: 04, 页码: 738-744
Authors:
彭俊
;
马嘉文
;
杨鹏飞
;
胡宗民
Adobe PDF(4986Kb)
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View/Download:347/85
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Submit date:2021/04/19
斜爆轰发动机
波系结构
临界条件
受限空间
激波反射
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)
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View/Download:291/62
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
斜爆轰发动机的推力性能理论分析
期刊论文
力学学报, 2021, 卷号: 53, 期号: 10, 页码: 2853-2864
Authors:
杨鹏飞
;
张子健
;
杨瑞鑫
;
滕宏辉
;
姜宗林
Adobe PDF(1224Kb)
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Submit date:2022/03/16
斜爆轰波
发动机
推力性能
燃烧模式
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)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:
Wang Q(汪球)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2057Kb)
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View/Download:268/83
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Submit date:2020/08/26
Shock tunnel
Detonation driver
Diaphragm
Dual ignition
High-enthalpy flow
斜爆轰的多波结构及其稳定性研究进展
期刊论文
力学进展, 2020, 卷号: 50, 期号: 1, 页码: 50-92
Authors:
滕宏辉
;
姜宗林
Adobe PDF(15005Kb)
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Submit date:2021/02/01
oblique detonation
shock
deflagration
initiation
stability
斜爆轰
激波
爆燃波
起爆
稳定性