关键词: 引射喷管;性能分析;喷管气流;试验;喷气式垂直起落飞机

Abstract: An analytical method for computing the performance of thrust augmentation ejector at primary flow pressure ratio above choking point and some experimental results of scale ejector model are presented in this paper.The comparison between the computational results of the performance by this method and the experimental data indicate a very good agreement.

Key words: Shrouded nozzle;Performance analysis;Nozzle flow;Experiment;Jet VTOL aircraft