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Numerical Study on Combustion Performance of Multi-Pintle Injector for Annular Combustor

  • Yaming Zhao
  • , Nanjia Yu*
  • , Yuhao Liu
  • *此作品的通讯作者
  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper presents a numerical study of an annular combustor with eight adjustable pintle injectors as injection units. Liquid oxygen and kerosene are used as propellants in the combustor, and the study focuses on analyzing its combustion performance under different throttle settings, turbulence ring structures, and additive gases. The results indicate that the combustor can achieve efficient combustion at both 10% and 100% throttle settings, but combustion efficiency decreases as the flow rate decreases. The turbulence ring structure can significantly improve the temperature distribution at the outlet. The higher, wider, and closer the turbulence structure is to the injector, the more uniform the temperature distribution becomes. Adding hydrogen can significantly reduce soot concentration, while the effect of water vapor is poor. A water vapor addition of more than 1.5% is required to achieve soot suppression, and nitrogen has almost no effect on soot suppression.

源语言英语
主期刊名Moving Integrated Product Development to Service Clouds in the Global Economy - Proceedings of the 21st ISPE Inc. International Conference on Concurrent Engineering, CE 2014
编辑Xuelin Lei
出版商IOS Press BV
623-635
页数13
ISBN(电子版)9781643686479
DOI
出版状态已出版 - 3 3月 2026
活动16th International Conference of Mechanical and Aerospace Engineering, ICMAE 2025 - Rome, 意大利
期限: 15 7月 202518 7月 2025

出版系列

姓名Advances in Transdisciplinary Engineering
87
ISSN(印刷版)2352-751X
ISSN(电子版)2352-7528

会议

会议16th International Conference of Mechanical and Aerospace Engineering, ICMAE 2025
国家/地区意大利
Rome
时期15/07/2518/07/25

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