摘要
基于国军标和适航标准对发动机冷却系统的验证要求,分析发动机短舱冷却系统在军机设计定型和民机适航取证试飞方面的不同,有助于我国军用航空发动机设计定型和大型民用发动机取证试飞水平的提升。
Aecording to test requirement ahout engine nacelle cooling system of military and civil airplanes provided in military specifications and airworthiness regulations, analyses the differences of engine cooling system test method in type qualification flight test between military airplane and civil airplane. It benefits to advance flight test technology in military engine type qualification and big civil airplane certification.
出处
《现代机械》
2013年第5期23-27,共5页
Modern Machinery
