摘要
以某型民用飞机再循环系统为研究对象,考察了从再循环系统到货舱和混合腔的流量分配。采用Flowmaster软件对再循环系统进行建模,对飞机在高空巡航和地面热天两种工况下的再循环系统流量分配进行了仿真计算。结果表明,该再循环系统的设计满足下游用户的流量需求。
This thesis investigates into recirculation system of certain civil aircraft and its flow split into cargo compartment and mix manifold. The software Flowmaster was introduced to build up mathematical model, and simulation analysis was performed for cruise and ground hot-day cases. It turns out the design of the recirculation system satisfies flow requirement from its downstream users.
出处
《民用飞机设计与研究》
2017年第2期131-134,共4页
Civil Aircraft Design & Research
