某型尾吊高平尾飞机失速特性试飞方法研究  

Research on Flight Test Methods of Stall Characteristics of a Rear-Mount Engine and High Horizontal Tail Civil Airplane

作　　者：邹灿东[1] 王育平[1] 徐南波[1] 付琳[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2012年第4期19-22,共4页Civil Aircraft Design & Research

摘　　要：某型尾吊高平尾飞机通过安装失速保护系统改善失速特性,满足了适航条例的要求。介绍了失速保护系统的设计,从保障试飞安全的失速试飞准备工作、失速保护系统研制试飞与失速特性验证试飞三个方面研究了安装失速保护系统飞机的失速试飞方法。Stall characteristics ot a rear-mourn engine airworthiness requirements are met by implementing stall protection system. The design of stall protection system is presented. Stall characteristics flight test methods of airplane with stall protection system are studied, including preparations for the flight test safety before stall flight test, stall protection system development flight test and airworthiness certification test.

关 键 词：尾吊高平尾飞机 失速特性 失速保护系统 试飞方法 

分 类 号：V217.3[航空宇航科学与技术—航空宇航推进理论与工程]