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Gust Alleviation of Aeroelastic Aircraft Using CFD Simulation

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000030" target="_blank" >RIV/00010669:_____/18:N0000030 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.sciencedirect.com/science/article/pii/S2352146518300371" target="_blank" >https://www.sciencedirect.com/science/article/pii/S2352146518300371</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.trpro.2018.02.033" target="_blank" >10.1016/j.trpro.2018.02.033</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Gust Alleviation of Aeroelastic Aircraft Using CFD Simulation

  • Original language description

    A CFD study of a gust alleviation technique based on the use of aircraft’s control surfaces on the main wing and on the horizontal tail plane is presented. The NASA Common Research model of an airliner is used as the reference configuration. The gust model is based on adding artificial gust velocities into the governing equations, so-called Disturbance Velocity Approach. The gust is identified as a change in the Angle of Attack upstream of the aircraft nose. A series of gusts is used to measure response of the aircraft and to establish the dynamic gust model. The elasticity of the aircraft model is taken into account employing modal analysis and the response of the aircraft structure is studied. The movable control surfaces are defined and characterized by CFD using the mesh deformation technique in the unsteady RANS simulations. Finally, the dynamic model based on both the gust data on one hand and on the control surfaces on the other is exploited to define the controller with the aim to alleviate the gust. The required time response of the movable control surfaces is studied to clarify limits of this alleviation technique.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2018

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    Transportation Research Procedia

  • ISBN

  • ISSN

    2352-1457

  • e-ISSN

    2352-1465

  • Number of pages

    10

  • Pages from-to

    366-375

  • Publisher name

    Elsevier Science B.V.

  • Place of publication

    Neuveden

  • Event location

    Bukurešť, Rumunsko

  • Event date

    Oct 16, 2017

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article

    000454701600033