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Z—8横侧稳定性和操纵性的飞行试验研究
引用本文:王新科.Z—8横侧稳定性和操纵性的飞行试验研究[J].飞行力学,1991(2):63-68.
作者姓名:王新科
作者单位:中国飞行试验研究院
摘    要:本文介绍了Z-8横侧稳定性和操纵性飞行试验的原理、方法和数据处理技术。给出了换算到标准条件下的试验结果,并与军用直升机飞行品质规范HB6105-86的有关要求进行了比较,并得出了结论。

关 键 词:直升机  稳定性  操纵性  飞行试验

FLIGHT TEST INVESTIGATION OF THE LATERAL-DIRECTIONAL STABILITY AND CONTROL OF THE Z-8 HELICOPTER
Wang Xinke.FLIGHT TEST INVESTIGATION OF THE LATERAL-DIRECTIONAL STABILITY AND CONTROL OF THE Z-8 HELICOPTER[J].Flight Dynamics,1991(2):63-68.
Authors:Wang Xinke
Institution:Chinese Flight Test Establishment
Abstract:This paper presents the principle, method and data processing technique of the flight test of the lateral-directional stability and control of the Z-8 helicopter. The test results converted under standard conditions are given and compared with the relative requirements of the military helicopter flying quality specification HB6105-86. Lastly, the objective and reasonable conclusions have been drawn.
Keywords:helicopter  stability  control
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