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

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 002
    Author:
    Konstantin I. Matveev
    DOI: 10.1061/(ASCE)AS.1943-5525.0000126
    Publisher: American Society of Civil Engineers
    Abstract: 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 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.
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      Heave-Pitch Motions of a Platform Flying in Extreme Ground Effect

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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian