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State Key... [21]
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姜宗林 [21]
刘云峰 [9]
张子健 [6]
韩桂来 [6]
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Funding Organization:National Natural Science Foundation of China
Document Type:期刊论文
Author:姜宗林
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Experimental study on the effects of the cone nose-tip bluntness
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 10, 页码: 7
Authors:
Liu MK(刘美宽)
;
Han GL(韩桂来)
;
Li, Zongxian
;
Jiang ZL(姜宗林)
Adobe PDF(2020Kb)
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Submit date:2022/12/29
An experimental study of formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2022, 卷号: 237, 页码: 5
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Yuan CK(苑朝凯)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(865Kb)
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View/Download:340/49
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Submit date:2022/02/17
Experimental study on the evolution of mode waves in laminar boundary layer on a large-scale flat plate
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 1, 页码: 16
Authors:
Liu MK(刘美宽)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(5472Kb)
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View/Download:335/56
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Submit date:2022/03/05
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 YF(刘云峰)
;
Wang C(王春)
Adobe PDF(15045Kb)
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View/Download:282/32
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Submit date:2022/01/24
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)
Adobe PDF(4805Kb)
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View/Download:362/72
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Submit date:2022/01/12
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:260/43
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Submit date:2021/11/01
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)
Adobe PDF(1806Kb)
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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)
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View/Download:297/60
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
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)
Adobe PDF(3790Kb)
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View/Download:438/79
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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View/Download:408/95
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation