000003287 001__ 3287
000003287 005__ 20141118153404.0
000003287 04107 $$acze
000003287 046__ $$k2005-05-09
000003287 100__ $$aHoráček, J.
000003287 24500 $$aDynamic and stability properties of an aeroelastic model

000003287 24630 $$n11.$$pENGINEERING MECHANICS 2005
000003287 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Brno
000003287 506__ $$arestricted
000003287 520__ $$2eng$$aFrequency modal and damping characteristics of an aeroelastic model designed for experiments in the wind tunnel are studied. Based on the experimental modal analysis the structural mass damping and stiffness matrices of the model are determined by identification procedures. The stability boundaries, i.e. the critical flow velocity for the flutter instability of the model, were measured in the wind tunnel. The results are aimed for supporting the development of new numerical methods for aeroelastic computations.

000003287 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000003287 653__ $$a

000003287 7112_ $$aENGINEERING MECHANICS 2005$$cSvratka (CZ)$$d2005-05-09 / 2005-05-12$$gEM2005
000003287 720__ $$aHoráček, J.$$iVeselý, J.$$iKozánek, J.
000003287 8560_ $$ffischerc@itam.cas.cz
000003287 8564_ $$s1013115$$uhttps://invenio.itam.cas.cz/record/3287/files/Horacek-PT.pdf$$y
             Original version of the author's contribution as presented on CD, .
            
000003287 962__ $$r3238
000003287 980__ $$aPAPER