短艙
In this paper, the calculational methods of air flow through the general aircraft nacelles are established according to the structure characteristic and bleeding-exhaust form. 本文通過(guò)分析飛機(jī)發(fā)動(dòng)機(jī)短艙的結(jié)構(gòu)特點(diǎn)和引排氣形式，建立了飛機(jī)典型短艙冷氣流量的計(jì)算方法。
