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Combustion Hysteresis Phenomenon in a Dual-Mode Scramjet
期刊论文
AIAA JOURNAL, 2024, 页码: 14./通讯作者:Yao, Wei
Authors:
Wang, Yu
;
Yao W(姚卫)
;
Zhang, Zheng
;
Liu, Jianwen
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View/Download:32/0
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Submit date:2025/01/13
Combustion hysteresis
Dual-mode scramjet
Hydrogen fuels
IDDES
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10./通讯作者:Yue, Lianjie
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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Adobe PDF(3862Kb)
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View/Download:461/173
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Fan XJ(范学军)
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View/Download:198/0
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Submit date:2019/11/20
Combustion chemistry
Combustion dynamics
Dual
mode scramjet
Flame stabilization
Improved delayed detached eddy simulations
Overall reactions
Scramjet combustors
Shock
wave structures
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
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:472/150
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Submit date:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:695/282
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas