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
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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.
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页码：531 / 544
页数：14
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