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共轴式直升机舰面起降风限图计算

杨俊

海军航空工程学院学报2017,Vol.32Issue(1):149-153,5.
海军航空工程学院学报2017,Vol.32Issue(1):149-153,5.DOI:10.7682/j.issn.1673-1522.2017.01.009

共轴式直升机舰面起降风限图计算

Computation of Save Operation Envelope of a Coaxial Helicopter on Shipboard

杨俊1

作者信息

  • 1. 中国直升机设计研究所,江西景德镇333001
  • 折叠

摘要

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.

关键词

共轴直升机/飞行动力学/舰面起降/风限图

Key words

coaxial helicopter/flight dynamics/taking-off and landing on shipboard/save operating envelope

分类

航空航天

引用本文复制引用

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):149-153,5.

基金项目

部委科研基金资助项目(15-cpb-06) (15-cpb-06)

海军航空工程学院学报

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