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Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer
Xue R(薛瑞)1,2; Zheng X1; Yue LJ(岳连捷)2; Zhang SK3; Weng C4
通讯作者Xui, Rui(ruixue@xjtu.edu.cn)
发表期刊INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
2020-06-08
卷号45期号:31页码:15683-15696
ISSN0360-3199
摘要A numerical study is carried out to investigate the shock train/flame interaction and skin friction with boundary layer combustion in compressible boundary layer. The Transition k - kl - w model is employed as the turbulence model and the finite-rate model is selected as the combustion model. The results showed that the skin friction could be reduced by 50% through boundary layer combustion while the pure-mixing case can only bring about a 10% drag reduction. The ignition of hydrogen in the boundary layer leads to a rapid reduction in skin friction. When a shock wave intersects with the flame surface, in addition to the reflection, it is also refracted, which will cause the change of both skin friction and heat transfer to the wall. Studies on the effects of air/fuel temperature ratio reveal that both the skin friction and heat transfer increase with air/fuel temperature ratio. When the concentration of H2O increases in airflow, the skin friction is enhanced as the mixing and combustion between oxygen and hydrogen is suppressed with H2O addition. The results of changing the air/fuel pressure ratios show that at high airflow pressure, the distance between the flame and the wall is reduced, leading to increase of heat transfer to the wall. (C) 2020 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
关键词Compressible boundary layer combustion Skin-friction reduction Shock train/flame interaction
DOI10.1016/j.ijhydene.2020.04.027
收录类别SCI ; EI
语种英语
WOS记录号WOS:000537629500024
关键词[WOS]SUPERSONIC COMBUSTION ; RAMJET PROPULSION ; FLOW ; SIMULATION ; INJECTION
WOS研究方向Chemistry ; Electrochemistry ; Energy & Fuels
WOS类目Chemistry, Physical ; Electrochemistry ; Energy & Fuels
资助项目National Natural Science Foundation of China[51706170] ; China Postdoctoral Science Foundation[2019TQ0246] ; China Postdoctoral Science Foundation[2019M663734] ; Foundation of State Key Laboratory of Coal Combustion (FSKLCCA2004) ; Natural Science Basic Research Program of Shaanxi[2020JQ-007] ; Foundation of State Key Laboratory of High Temperature Gas Dynamics ; Fundamental Research Funds for the Central Universities[xzy012019053] ; Fundamental Research Funds for the Central Universities[xjh012019033] ; Foundation of State Key Laboratory of Turbulence & Complex Systems
项目资助者National Natural Science Foundation of China ; China Postdoctoral Science Foundation ; Foundation of State Key Laboratory of Coal Combustion (FSKLCCA2004) ; Natural Science Basic Research Program of Shaanxi ; Foundation of State Key Laboratory of High Temperature Gas Dynamics ; Fundamental Research Funds for the Central Universities ; Foundation of State Key Laboratory of Turbulence & Complex Systems
论文分区二类
力学所作者排名1
RpAuthorXui, Rui
引用统计
被引频次:8[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
条目标识符http://dspace.imech.ac.cn/handle/311007/82117
专题高温气体动力学国家重点实验室
作者单位1.Xi An Jiao Tong Univ, Sch Aerosp, State Key Lab Strength & Vibrat Mech Struct, Shaanxi Engn Lab Vibrat Control Aerosp Struct, Xian 710049, Peoples R China;
2.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;
3.Xian Modern Control Technol Res Inst, Xian 710065, Peoples R China;
4.Tongji Univ, Shanghai 200092, Peoples R China
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GB/T 7714
Xue R,Zheng X,Yue LJ,et al. Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer[J]. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,2020,45,31,:15683-15696.
APA 薛瑞,Zheng X,岳连捷,Zhang SK,&Weng C.(2020).Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer.INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,45(31),15683-15696.
MLA 薛瑞,et al."Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer".INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 45.31(2020):15683-15696.
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