Direct dynamic response computation of an aircraft structure based on experimentally identified modal model

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001838" target="_blank" >RIV/00010669:_____/14:#0001838 - 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
Direct dynamic response computation of an aircraft structure based on experimentally identified modal model
Original language description
The paper presents a technique of dynamic response computation of an aircraft structure using modal model directly, without any need of FEM model and its costly tuning. The basis of the technique is a numerical solution of convolution integral in n?dimensional space. Excitation forces are supposed arbitrary waveforms.
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
30 th 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
77-78
Publisher name
University of West Bohemia
Place of publication
Plzeň
Event location
Hotel Horizont, Špičák
Event date
Jan 1, 2014
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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