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
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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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
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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