Y7H─500型飞机高速特性适航试飞  

AIRWORTHINESS CERTIFICATION FLIGHT TEST ABOUT HIGH-SPEED CHARACTERISTICS FOR Y7H─500 AIRPLANE

作　　者：霍建武 樊力 王启 

机构地区：[1]西安飞行试验研究院

出　　处：《飞行力学》1995年第1期56-61,共6页Flight Dynamics

摘　　要：根据民用飞机在投入营运之前，要按飞机适航标准进行适航取证试飞的要求，对Ｙ７Ｈ－５００型飞机进行了高速特性适航试飞验证。简要介绍了试验机概况、试飞方法和测试技术；讨论了Ｙ７Ｈ－５００型飞机的高速特性。试验结果表明，Ｙ７Ｈ－５００型飞机的高速特性符合ＣＣＡＲ－２５部要求。Before entering service , all the civil airplanes will have to conductairworthiness certification flight test according to airworthiness standards. This paper willbriefly introduce the test airplane 's general situation , flight test methods and measurementtechniques,discuss the high-speed characteristics of Y7H-500 airplane. The resultsindicate that the high-speed characteristics of Y7H-500 airplane meet the requirements ofPart 25 of China Civil Aviation Regulation (CCAR-25)

关 键 词：飞机 高速特性 飞机试验 突风颠倾 

分 类 号：V221.91[航空宇航科学与技术—飞行器设计]