摘要
根据“不变燃烧时滞”理论建立起单组元推进剂鱼雷燃烧室低频燃烧稳定性的控制方程 ,结合实际情况分析了影响单组元推进剂鱼雷燃烧室低频燃烧不稳定性的激励因素和鱼雷旋转燃烧室的热爆机理 。
In this paper, the controlling equation of monopropellant low frequency combustion stability in torpedo combustor is set up according to the theory of 'fixed combustion time lag'. The prompting factors that influenced monopropellant low frequency combustion instability in torpedo combustor and the heating explosion mechanism of torpedo rotary combustor are analyzed by combined with the fact. And the resolve measures are also proposed.
出处
《舰船科学技术》
北大核心
2003年第3期12-15,共4页
Ship Science and Technology
