Helicopter rotor aerodynamics and dynamics

被引：0
|
作者：
Gausz, T [1 ]
机构：
[1] Tech Univ Budapest, Dept Aircraft & Ships, H-1521 Budapest, Hungary
来源：
PROCEEDINGS OF THE 5TH MINI CONFERENCE ON VEHICLE SYSTEM DYNAMICS, IDENTIFICATION AND ANOMALIES | 1996年
关键词：
rotor aerodynamics; momentum theory; blade element theory;
D O I：
暂无
中图分类号：
U [交通运输];
学科分类号：
08 ; 0823 ;
摘要：
The present method deals with rotor dynamics and aerodynamics. The combined blade-element and momentum theory and the ONERA semi-empirical; model were applied in the aerodynamical calculations. The unsteady aerodynamic effects can be calculated by using the ONERA model. The equation of the napping motion was solved by applying the induced velocity field. So the generalised equilibrium path of the rotor blades was approximated with an asymptotic solution.
引用
收藏
页码：377 / 384
页数：8
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