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直升机回避区曲线的试验研究
引用本文:贾新哲,杨松山.直升机回避区曲线的试验研究[J].飞行力学,1996,14(2):65-69,74.
作者姓名:贾新哲  杨松山
摘    要:主要阐述直升机回避区曲线的试验确定方法,分析了影响回避区曲线的各种因素,导出了回避区曲线与直升机的自转性能,总距操纵应和着陆装置承受能力等参数的关系。该方法经飞行试验证明是切实可行的,可用于各种直升机的飞行试验,解决了新机试飞中的难题。

关 键 词:直升机  飞行试验  回避区  自转性能  总距操纵响应

^A Flight Test Method of Helicopter Dead Man's Curve
Jia Xinzhe, Yang Songshan.^A Flight Test Method of Helicopter Dead Man''''s Curve[J].Flight Dynamics,1996,14(2):65-69,74.
Authors:Jia Xinzhe  Yang Songshan
Institution:Chinese Flight Test Establishment
Abstract:A flight test method to determine the dead man's curve of the helicopterwas presented in this article. Some kinds of factors affecting the dead man's curve werediscussed. The relationship between dead man's curve and some parameters, such as autorotation performance, collective pitch response and carrying ability of land gear, wasderived in the paper. Compared with the result of helicopter flight test, the method isacceptable and can be used in some kinds of helicopter flight test.
Keywords:Flight test Dead man's curve Autorotation performanceCollective pitch response  
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