摘要
主动冷却是高超声速飞行器最主要的冷却方式,文章探讨了对流冷却结构主动热防护效率参数影响规律,为高超声速飞行器放热结构设计提供指导。
Active cooling is the most important cooling method for hypersonic vehicle. In this paper, the influence of active thermal protection efficiency parameters on convection cooling structure is discussed, which provides guidance for the design of heat release structure of hypersonic vehicle.
出处
《科技创新与应用》
2018年第18期53-54,共2页
Technology Innovation and Application
关键词
对流冷却结构
主动热防护
效率参数
影响
规律
convection cooling structure
active thermal protection
efficiency parameter
influence
regularity
