Updating of Aircraft Dynamic Model According Results of Ground Vibration Test

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001877" target="_blank" >RIV/00010669:_____/14:#0001877 - isvavai.cz</a>
Result on the web
<a href="http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" target="_blank" >http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Updating of Aircraft Dynamic Model According Results of Ground Vibration Test
Original language description
Submitted paper deals with an aircraft structure analytical dynamic model updating according to ground vibration tests (GVT) results. Paper describes possible approaches of flutter analysis as regards to the incorporation of GVT results. Then a theoretical background of the model updating methods are given. Next, the methodology of an aircraft structure dynamic model updating is described. Practical application is documented on the example of EV 55M turboprop utility aircraft model updating. Selected results of the symmetric model updating are shown. Finally, further usage of the updated model is outlined.
Czech name
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Czech description
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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
30th Conference with international Participation, Computational Mechanics 2014
ISBN
978-80-261-0429-2
ISSN
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e-ISSN
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Number of pages
2
Pages from-to
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Publisher name
Západočeská universita Plzeň
Place of publication
ČR
Event location
Špičák, ČR
Event date
Jan 1, 2014
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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