000009177 001__ 9177
000009177 005__ 20141204092415.0
000009177 04107 $$aeng
000009177 046__ $$k12/05/2014
000009177 100__ $$aChládek, Š.
000009177 24500 $$aNumerical simulation and experiment swith the profile NACA 0012

000009177 24630 $$n18.$$pEngineering Mechanics 2012
000009177 260__ $$bInstitute of Theoretical and Applied Mechanics, AS CR, Prague
000009177 506__ $$arestricted
000009177 520__ $$2eng$$aThis paper introduces the new model of the airfoil and describes both aeroelastic experiments and numerical simulation with the prof le NACA 0012. Mathematical description of the f uid-structure interaction has to involve both the equations of the f uid dynamic and the equations of motion of the solid body. The f rst results will be presented.

000009177 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000009177 653__ $$aaeroelastic, flow-structure interaction, identification

000009177 7112_ $$aEngineering Mechanics 2012$$cSvratka (CZ)$$d12/05/2014 - 15/05/2014$$gEM2012
000009177 720__ $$aChládek, Š.$$iZolotarev, I.$$iUruba, V.
000009177 8560_ $$ffischerc@itam.cas.cz
000009177 8564_ $$s359123$$uhttps://invenio.itam.cas.cz/record/9177/files/078_Chladek_S-FT.pdf$$yOriginal version of the author's contribution as presented on CD, paper (No. 078).
000009177 962__ $$r8924
000009177 980__ $$aPAPER