Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor
Joint Authors
Yang, Jun
Wu, Xian-yu
Wang, Zhen-guo
Source
International Journal of Aerospace Engineering
Issue
Vol. 2016, Issue 2016 (31 Dec. 2016), pp.1-14, 14 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2016-07-25
Country of Publication
Egypt
No. of Pages
14
Abstract EN
Generally, the overall performance of scramjet combustor is greatly impacted by the fuel distribution scheme.
The current paper mainly conducted a comprehensive parametric study of the impact of fuel distribution on the overall performance of a kerosene-based scramjet combustor.
Herein, a 3D supersonic combustor with a recessed cavity and four injection orifices was taken into consideration.
The combustor’s performance was analyzed by 3D RANS model.
The fuel equivalence ratio for each injection port was taken as the design variables.
And the combustion efficiency, the total pressure recovery coefficient, and the drag coefficient were chosen as the objective functions.
Some novel data mining methods including DOE technique, Kriging approximation model, interaction analysis, and main effects analysis methods were employed to conduct the parametric study.
The distributed fuel injection scheme was optimized by nondominated sorting genetic algorithm.
The results show that three objective functions were remarkably affected by both of the total fuel equivalence ratio and the fuel distribution scheme.
The objective functions cannot reach the optimal solution at the same time, and there must be a tradeoff among the objective functions.
American Psychological Association (APA)
Yang, Jun& Wu, Xian-yu& Wang, Zhen-guo. 2016. Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor. International Journal of Aerospace Engineering،Vol. 2016, no. 2016, pp.1-14.
https://search.emarefa.net/detail/BIM-1105025
Modern Language Association (MLA)
Yang, Jun…[et al.]. Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor. International Journal of Aerospace Engineering No. 2016 (2016), pp.1-14.
https://search.emarefa.net/detail/BIM-1105025
American Medical Association (AMA)
Yang, Jun& Wu, Xian-yu& Wang, Zhen-guo. Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor. International Journal of Aerospace Engineering. 2016. Vol. 2016, no. 2016, pp.1-14.
https://search.emarefa.net/detail/BIM-1105025
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1105025