| Citation: | WANG Jinjin, ZHA Bailin, ZHANG Wei, et al. Effect of air-inlet structures on combustion and flow field of inner wall in secondary combustion chamber of solid rocket ramjet[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(5): 989-998. doi: 10.13700/j.bh.1001-5965.2018.0525(in Chinese)
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In order to study the effect of air-inlet structures on combustion and ablation combustion chamber of solid ramjet, the flow field characteristics in the secondary in the secondary combustion chamber of solid rocket ramjet with bilateral 180° air-inlet structure and bilateral 90° air-inlet structure on both down sides were analyzed based on the standard
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