Influence of multi-strut interaction on flame propagation and combustion performance in a large aspect ratio combustor

被引:15
作者
Qiu, Hongchao [1 ]
Lin, Libo [1 ]
Zhang, Junlong [1 ]
Zhang, Shiqi [1 ]
Bao, Wen [1 ]
机构
[1] Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
Supersonic combustion; Liquid kerosene; Multi-strut; Flame propagation characteristics; Combustion performance; DUAL-MODE SCRAMJET; SUPERSONIC COMBUSTION; HYDROGEN; STABILIZATION; TRANSITION; FUEL; KEROSENE; CONFIGURATIONS; OPTIMIZATION; INJECTORS;
D O I
10.1016/j.ast.2023.108193
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The flame propagation characteristics and combustion performance of the multi-strut-equipped super-sonic combustor with a large aspect ratio fueled by liquid kerosene were observed to deepen understand-ing of the combustion characteristics. Some numerical simulations and experiments have been carried out at the condition of Tt = 1680 K, Pt = 1.64 MPa, and Ma = 2.7. The fuel distribution under different injection modes was analyzed, and it was found that the fuel mixing efficiency was 28.7% under the single-strut injection method. As the number of injection struts increased to 5, the fuel mixing efficiency improved to 53.8%. The interaction between the ignition strut flame and the injection strut flame was discussed. The results indicated that the fuel injected by the fuel injection strut could be ignited under a high-intensity ignition flame, and the ignition strut flame was promoted by the injection strut flame. The flame characteristics under different installation widths of the injection struts were analyzed. The fuel injected by the injection strut could not be ignited when the large installation width was 40.5 mm. A method to increase the flame spread width without the addition of extra energy was proposed based on the flame propagation characteristics. This method not only increases the flame width but also widens the combustion boundary. The principle of this method was revealed by analyzing the characteristics of the cross-flame. The results of this paper are beneficial for the future performance optimization of large aspect ratio combustors using liquid hydrocarbon fuel. (c) 2023 Published by Elsevier Masson SAS.
引用
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页数:12
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共 50 条
[1]   Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines [J].
Candon, M. J. ;
Ogawa, H. .
ACTA ASTRONAUTICA, 2018, 147 :281-296
[2]   Switching control of thrust regulation and inlet unstart protection for scramjet engine based on Min strategy [J].
Cao, Ruifeng ;
Chang, Juntao ;
Tang, Jingfeng ;
Bao, Wen ;
Yu, Daren ;
Wang, Zhongqi .
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 40 :96-103
[3]  
Chandrasekhar C., 2012, Int. J. Sci. Technol, V1, P671
[4]  
Choubey G., 2016, Perspect Sci, V8, P222
[5]   Numerical investigation on geometric sensitivity and flame stabilisation mechanism in H2 fueled two-strut based scramjet combustor [J].
Choubey, Gautam ;
Gaud, Parth ;
Fatah, Abdulnasser Mahmood ;
Devarajan, Yuvarajan .
FUEL, 2022, 312
[6]   Hydrogen fuel in scramjet engines - A brief review [J].
Choubey, Gautam ;
Yuvarajan, D. ;
Huang, Wei ;
Yan, Li ;
Babazadeh, Houman ;
Pandey, K. M. .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 45 (33) :16799-16815
[7]   Effect of different wall injection schemes on the flow-field of hydrogen fuelled strut-based scramjet combustor [J].
Choubey, Gautam ;
Pandey, K. M. .
ACTA ASTRONAUTICA, 2018, 145 :93-104
[8]  
Choubey G, 2017, MATER TODAY-PROC, V4, P2608, DOI 10.1016/j.matpr.2017.02.115
[9]   Large Eddy Simulation of a supersonic air ejector [J].
Croquer, Sergio ;
Lamberts, Olivier ;
Poncet, Sebastien ;
Moreau, Stephane ;
Bartosiewicz, Yann .
APPLIED THERMAL ENGINEERING, 2022, 209
[10]   The heat flux research in hydrogen supersonic combustor at Mach number of 4 [J].
Goldfeld, Marat .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 46 (24) :13365-13376