收稿日期:
2023-08-16
修回日期:
2023-09-11
接受日期:
2023-11-20
出版日期:
2024-06-15
发布日期:
2023-12-07
通讯作者:
谭永华
E-mail:tanyhcasc@163.com
基金资助:
Guangxu WANG1, Bin LI1,2, Yonghua TAN1,2(), Yushan GAO1
Received:
2023-08-16
Revised:
2023-09-11
Accepted:
2023-11-20
Online:
2024-06-15
Published:
2023-12-07
Contact:
Yonghua TAN
E-mail:tanyhcasc@163.com
Supported by:
摘要:
高频燃烧不稳定现象诱发的大幅值压力振荡严重威胁液体火箭发动机可靠性,为此,国内外开展了大量深入的研究工作。为了提高对此类问题及相关研究的整体认识,系统阐述了液体火箭发动机高频燃烧不稳定问题的主要特点、关键物理机制、研究思路等,重点梳理了国内外在液体推进剂燃烧子过程响应机理方面的研究工作,明确指出了燃烧速率控制过程对于此类问题分析的重要意义。在此基础上,详细总结了液滴蒸发和射流掺混作为速率控制过程的高频燃烧不稳定问题数值仿真研究进展,仔细归纳了线性和非线性理论解析分析方法面临的挑战,简要介绍了基于非线性动力系统的分析方法在揭示高频燃烧不稳定非线性行为以及稳定性裕度评估方面的重要潜力。最后,针对不同工程控制措施的内在联系、应用情况等进行了分析,特别强调了燃烧释热分布控制的重要性。
中图分类号:
汪广旭, 李斌, 谭永华, 高玉闪. 液体火箭发动机高频燃烧不稳定问题综述[J]. 航空学报, 2024, 45(11): 529450-529450.
Guangxu WANG, Bin LI, Yonghua TAN, Yushan GAO. High frequency combustion instability in liquid rocket engines: Review[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(11): 529450-529450.
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