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Open-loop control of combustion instabilities in a full-scale annular ramjet combustor using linear genetic programming

Jianguo TAN Zheng XU Yao LIU Dongdong ZHANG Yi HOU

中国航空学报(英文版)2026,Vol.39Issue(2):20-28,9.
中国航空学报(英文版)2026,Vol.39Issue(2):20-28,9.DOI:10.1016/j.cja.2025.103744

Open-loop control of combustion instabilities in a full-scale annular ramjet combustor using linear genetic programming

Open-loop control of combustion instabilities in a full-scale annular ramjet combustor using linear genetic programming

Jianguo TAN 1Zheng XU 1Yao LIU 2Dongdong ZHANG 1Yi HOU1

作者信息

  • 1. Hypersonic Technology Laboratory,National University of Defense Technology,Changsha 410073,China
  • 2. Beijing Institute of Tracking and Telecommunications Technology,Beijing 100094,China
  • 折叠

摘要

关键词

Annular ramjet combustor/Combustion instabilities/Linear genetic programming/Machine learning/Open-loop control

Key words

Annular ramjet combustor/Combustion instabilities/Linear genetic programming/Machine learning/Open-loop control

引用本文复制引用

Jianguo TAN,Zheng XU,Yao LIU,Dongdong ZHANG,Yi HOU..Open-loop control of combustion instabilities in a full-scale annular ramjet combustor using linear genetic programming[J].中国航空学报(英文版),2026,39(2):20-28,9.

基金项目

The authors would like to express their thanks for the support from the National Natural Science Foundation of China(No.12002372) (No.12002372)

the Young Elite Scientists Sponsorship Program by China Association for Science and Technology(No.2022QNRC001) (No.2022QNRC001)

the Natural Science Foundation of Hunan Province,China(No.2021JJ40674). (No.2021JJ40674)

中国航空学报(英文版)

1000-9361

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