Heave-Pitch Motions of a Platform Flying in Extreme Ground Effect

被引:5
|
作者
Matveev, Konstantin I. [1 ]
机构
[1] Washington State Univ, Sch Mech & Mat Engn, Pullman, WA 99164 USA
基金
美国国家科学基金会;
关键词
Vehicle dynamics; Motion stability; Wing-in-ground craft; Extreme ground effect;
D O I
10.1061/(ASCE)AS.1943-5525.0000126
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
High-payload platforms flying in extreme-ground-effect represent a promising concept for high-speed amphibious transportation. Their dynamics is governed, to a large extent, by unsteady airflow under the platform. A quasi-one-dimensional model for the underplatform channel-flow is applied to predict heave and pitch motions of a vehicle in the presence of external disturbances, such as nonuniformities on the underlying ground-surface. It is found that a complete nonlinear theory should be used instead of a linear model to accurately predict motions when ground nonuniformities are relatively short. A flat platform with a flap moving in extreme-ground-effect is intrinsically unstable. An aftwing out of ground-effect can be added to the system to achieve stability. Movable control surfaces, such as a platform flap, can be also modeled by the nonlinear theory. It is demonstrated that an oscillating flap can reduce heave and pitch amplitudes in flight over a wavy ground-surface. DOI: 10.1061/(ASCE)AS.1943-5525.0000126. (C) 2012 American Society of Civil Engineers.
引用
收藏
页码:238 / 245
页数:8
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