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共轴式直升机舰面起降风限图计算
引用本文:杨俊.共轴式直升机舰面起降风限图计算[J].海军航空工程学院学报,2017,32(1):149-160.
作者姓名:杨俊
作者单位:中国直升机设计研究所,江西景德镇333001
摘    要:通过建立共轴双旋翼直升机的舰面起降飞行动力学模型,计算了某型共轴双旋翼直升机在某型舰上的起降特性。根据相关判据,得出该机舰组合的起降风限图。起降风限图为该直升机在舰上的安全起降提供了指导,有重要的实际意义。

关 键 词:共轴直升机  飞行动力学  舰面起降  风限图

Computation of Save Operation Envelope of a Coaxial Helicopter on Shipboard
YANG Jun.Computation of Save Operation Envelope of a Coaxial Helicopter on Shipboard[J].Journal of Naval Aeronautical Engineering Institute,2017,32(1):149-160.
Authors:YANG Jun
Affiliation:China Helicopter Research and Development Institute, Jingdezhen Jiangxi 333001, China
Abstract:This paper sets up a flight dynamic model of a coaxial helicopter and, computes the take-off and landing charac? teristics on shipboard. Finally, the safe operating envelope (SOE) for the combination of the very helicopter and ship was obtained, according to some criterions. The SOE provided a guidance for helicopter safely taking-off and landing on ship, which was significant in practice.
Keywords:coaxial helicopter  flight dynamics  taking-off and landing on shipboard  save operating envelope
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