A THEORETICAL-MODEL FOR PREDICTING THE BLADE SAILING BEHAVIOR OF A SEMIRIGID ROTOR HELICOPTER

被引：0

作者：

NEWMAN, SJ

机构：

来源：

VERTICA | 1990年 / 14卷 / 04期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A theoretical aeroelastic model has been developed for determining the blade flapwise motion of a helicopter rotor during rotor engagement and disengagement, particularly in high wind conditions during operation from the flight deck of a ship. A computer program has been written and results from it are presented for a Lynx helicopter. Details of the flow state over typical flight deck are provided by wind tunnel tests of a 1/120th scale model of a ship of the Rover class of the Royal Fleet Auxiliary.

引用

页码：531 / 544

页数：14

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