论文类型：期刊论文
论文编号：404099
发表刊物：Journal of Beijing University of Aeronautics and Astronautics
卷号：52
期号：6
页面范围：2000-2010
ISSN号：1001-5965
关键字：Combustion performance prediction; Integrated afterburner; Large eddy simulation; Machine learning; Recirculation zone; Thermal flow field