Numerical research on flow and performance of adaptive throat combustor for wide-range scramjetOA

作者：Shengzu GUO;Xu ZHANG;Fangyou YU;Hao CHEN;Qifan ZHANG;Lianjie YUE

作者单位：State Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China||School of Engineering Science,University of Chinese Academy of Sciences,Beijing 100049,ChinaState Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,ChinaState Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China||School of Engineering Science,University of Chinese Academy of Sciences,Beijing 100049,ChinaState Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,ChinaState Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,ChinaState Key Laboratory of High Temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China||School of Engineering Science,University of Chinese Academy of Sciences,Beijing 100049,China

中文关键词：Geometric throatScramjetStaged combustorThermal throatWide speed range

英文关键词：Geometric throatScramjetStaged combustorThermal throatWide speed range

刊名：《中国航空学报（英文版）》 2026 (8)

页码/页数：213-230,18

基金：This work was supported by the National Natural Science Foundation of China(Nos.U2141220,12372236,U2341240 and 12302392).

DOI：10.1016/j.cja.2025.103861