AN APPROXIMATE THEORETICAL APPROACH FOR THE DETERMINATION OF OSCILLATORY AERODYNAMIC COEFFICIENTS FOR A HELICOPTER ROTOR IN FORWARD FLIGHT

被引：0
|
作者：
MOLYNEUX, WG
机构：
来源：
AERONAUTICAL QUARTERLY | 1962年 / 13卷 / 03期
关键词：
D O I：
10.1017/S0001925900002456
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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收藏
页码：235 / 254
页数：20
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