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力学研究所 [7]
工程热物理研究所 [2]
清华大学 [1]
北京航空航天大学 [1]
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期刊论文 [9]
会议论文 [2]
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Standing oblique detonation for hypersonic propulsion: A review
期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
作者:
Jiang ZL(姜宗林)
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浏览/下载:0/0
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提交时间:2024/02/26
Standing oblique detonation
Scramjet engine
Oblique detonation engine
Shock wave
Supersonic combustion
Hypersonic ramjet propulsion
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
作者:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
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  |  
浏览/下载:11/0
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提交时间:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
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
作者:
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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浏览/下载:50/0
  |  
提交时间:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
雾霾中的雾对盐密的影响
期刊论文
2016, 2016
马德英
;
刘动
;
卢明
;
陈枫林
;
MA Deying
;
LIU Dong
;
LU Ming
;
CHEN Fenglin
收藏
  |  
浏览/下载:4/0
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
作者:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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  |  
浏览/下载:14/0
  |  
提交时间:2016/09/14
Dual-mode scramjet
Engine performance
Thrust
Optimization
Heat release distribution
Simulated annealing algorithm
Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine
期刊论文
COMBUSTION THEORY AND MODELLING, 2014, 卷号: 18, 页码: 652-691
作者:
Gao, Zhenxun
;
Wang, Jingying
;
Jiang, Chongwen
;
Lee, Chunhian
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浏览/下载:2/0
  |  
提交时间:2020/01/06
compressibility effect
finite rate model
supersonic turbulent combustion
scramjet engine
flamelet model
Theoretical analysis of effects of boundary layer bleed on scramjet thrust
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
作者:
Yue LJ(岳连捷)
;
Xu XK(徐显坤)
;
Zhang XY(张新宇)
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浏览/下载:15/0
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提交时间:2013/10/23
scramjet
boundary layer bleed
theoretical analysis
engine thrust
Performance of the fuel injector in supersonic combustor
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
作者:
Wei Z(卫喆)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Gu SL(顾声龙)
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  |  
浏览/下载:16/0
  |  
提交时间:2017/07/14
Concentration profiles
Engine design
Fuel injectors
Fuel-air mixing
Gas sampling
Ramp injector
Scramjet combustors
Scramjet test
Supersonic combustors
Experimental investigation of cavity-based scramjet model
会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者:
Gu HB(顾洪斌)
;
Chen LH(陈立红)
;
张新宇(Chang XY)
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2017/06/01
Kerosene fuel
Mass flow rate
Scramjet engine
The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor
期刊论文
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 371,380
Mohammad Ali
;
S. Ahmed
;
A.K.M. Sadrul Islam
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  |  
浏览/下载:11/0
  |  
提交时间:2013/03/12
scramjet engine
TVD scheme
finite width of inlet
supersonic mixing
parallel air stream
flame holding.
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