Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor
المؤلفون المشاركون
Yang, Jun
Wu, Xian-yu
Wang, Zhen-guo
المصدر
International Journal of Aerospace Engineering
العدد
المجلد 2016، العدد 2016 (31 ديسمبر/كانون الأول 2016)، ص ص. 1-14، 14ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2016-07-25
دولة النشر
مصر
عدد الصفحات
14
الملخص 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.
نمط استشهاد جمعية علماء النفس الأمريكية (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
نمط استشهاد الجمعية الأمريكية للغات الحديثة (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
نمط استشهاد الجمعية الطبية الأمريكية (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
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1105025
قاعدة معامل التأثير والاستشهادات المرجعية العربي "ارسيف Arcif"
أضخم قاعدة بيانات عربية للاستشهادات المرجعية للمجلات العلمية المحكمة الصادرة في العالم العربي
تقوم هذه الخدمة بالتحقق من التشابه أو الانتحال في الأبحاث والمقالات العلمية والأطروحات الجامعية والكتب والأبحاث باللغة العربية، وتحديد درجة التشابه أو أصالة الأعمال البحثية وحماية ملكيتها الفكرية. تعرف اكثر