Using swirl atomizer designed by this paper , kerosene was injected into the ejector combustor , and achieved steady combustion . this made a solid foundation for the future study on combustion organization 設(shè)計(jì)了旋流式霧化噴嘴,實(shí)現(xiàn)了煤油在引射火箭模態(tài)中的穩(wěn)定燃燒,為進(jìn)一步的燃燒組織研究奠定了基礎(chǔ)。