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contributor authorKonstantin I. Matveev
date accessioned2017-05-08T21:33:50Z
date available2017-05-08T21:33:50Z
date copyrightApril 2012
date issued2012
identifier other%28asce%29as%2E1943-5525%2E0000126.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56270
description abstractHigh-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 aft-wing 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.
publisherAmerican Society of Civil Engineers
titleHeave-Pitch Motions of a Platform Flying in Extreme Ground Effect
typeJournal Paper
journal volume25
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000126
treeJournal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 002
contenttypeFulltext


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