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姜宗林 [4]
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基于主动射流控制的高超声速进气道再起动性能研究(英文)
期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:
靳一超
;
姚卫
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Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
碳氢燃料超声速燃烧分区实验研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 06, 页码: 1533-1547
Authors:
孟凡钊
;
周芮旭
;
李忠朋
;
连欢
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Submit date:2022/08/11
超声速燃烧
香农熵
燃烧特征时间
燃烧分区
提高高马赫数超燃冲压发动机推力的理论方法
期刊论文
力学学报, 2022, 卷号: 54, 期号: 03, 页码: 633-643
Authors:
韩信
;
刘云峰
;
张子健
;
张文硕
;
马凯夫
Adobe PDF(1617Kb)
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Submit date:2022/06/10
高马赫数超燃冲压发动机
斜爆轰发动机
激波诱导燃烧冲压发动机
超声速燃烧
提高推力的方法
高马赫数超燃冲压发动机技术研究进展
期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:
岳连捷
;
张旭
;
张启帆
;
陈科挺
;
李进平
;
陈昊
;
姚卫
;
仲峰泉
;
李飞
;
王春
;
陈宏
Adobe PDF(2622Kb)
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Submit date:2022/03/16
高马赫数
超燃冲压发动机
热化学非平衡
超声速燃烧
低雷诺数流动
激波风洞
飞行试验
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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Submit date:2021/04/19
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)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
斜爆轰发动机燃烧机理试验研究
期刊论文
推进技术, 2021, 卷号: 42, 期号: 04, 页码: 786-794
Authors:
张子健
;
韩信
;
马凯夫
;
张文硕
;
刘云峰
;
苑朝凯
;
姜宗林
Adobe PDF(6817Kb)
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Submit date:2021/04/19
斜爆轰发动机
超声速燃烧
激波诱导燃烧
斜爆轰波
斜激波
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
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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
Aerothermal characteristics of bleed slot in hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:
Yue LJ(岳连捷)
;
Lu HB
;
Xu X
;
Chang XY
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
Radical recombination in a hydrocarbon-fueled scramjet nozzle
期刊论文
Chinese Journal of Aeronautics, 2014, 卷号: 27, 期号: 6, 页码: 1413-1420
Authors:
Zhang XY(张晓源)
;
Qin LZ
;
Chen H(陈宏)
;
He XZ
;
Liu Y
;
Qin, LZ (reprint author), Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China.
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Submit date:2015/03/11
Chemical Reactions
Nozzles
Performance Calculation
Radical
Recombination