000003187 001__ 3187
000003187 005__ 20141118153408.0
000003187 04107 $$acze
000003187 046__ $$k2014-11-03
000003187 100__ $$aMalínek, P.
000003187 24500 $$aDirect dynamic response computation of an aircraft structure based on experimentally identified modal model

000003187 24630 $$n30.$$pCOMPUTATIONAL MECHANICS 2014 / Book of extended abstracts
000003187 260__ $$bUniversity of West Bohemia, Plzeň, Czech Republic
000003187 506__ $$arestricted
000003187 520__ $$2eng$$a

000003187 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000003187 653__ $$a

000003187 7112_ $$a30th conference COMPUTATIONAL MECHANICS 2014 and the workshop Modelling and Inverse Problems for Heterogeneous Media$$cŠpičák (CZ)$$d2014-11-03 / 2014-11-05$$gCM2014
000003187 720__ $$aMalínek, P.
000003187 8560_ $$ffischerc@itam.cas.cz
000003187 8564_ $$s496765$$uhttps://invenio.itam.cas.cz/record/3187/files/page_0077.pdf$$y
             Original version of the author's contribution as presented on CD, , page 77.
            
000003187 962__ $$r3058
000003187 980__ $$aPAPER