000008907 001__ 8907
000008907 005__ 20141204083531.0
000008907 04107 $$aeng
000008907 046__ $$k12/05/2014
000008907 100__ $$aVlček, V.
000008907 24500 $$aFLUTTER AT A LOW VELOCITY

000008907 24630 $$n20.$$pEngineering Mechanics 2014
000008907 260__ $$bBrno University of Technology- Institute of Solid Mechanics, Mechatronics and Biomechanics
000008907 506__ $$arestricted
000008907 520__ $$2eng$$aAeroelastic experiments with the profile NACA0015 were realized in the suction type aerodynamic tunnel of the Institute of Thermomechanics, Czech Academy of Sciences, Prague. The profile had two degrees of freedom realized in translation and rotation motion and flow velocity was just up its critical value. The flow field was measured with interferometry method and the results obtained at the velocity M = 0.23 in the flutter regime are presented. The evaluation of interferogramms enabled to determine the components of the drag and lift forces.

000008907 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000008907 653__ $$aAeroelasticity, Flutter, Interferometry, Subsonic flow.

000008907 7112_ $$aEngineering Mechanics 2014$$cSvratka (CZ)$$d12/05/2014 - 15/05/2014$$gEM2014
000008907 720__ $$aVlček, V.$$iKozánek, J.$$iZolotarev, I.
000008907 8560_ $$ffischerc@itam.cas.cz
000008907 8564_ $$s347710$$uhttps://invenio.itam.cas.cz/record/8907/files/162-Vlcek-CD.pdf$$yOriginal version of the author's contribution as presented on CD, paper No. 162.
000008907 962__ $$r70
000008907 980__ $$aPAPER