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
引用
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页码:235 / 254
页数:20
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