000001704 001__ 1704
000001704 005__ 20141118153457.0
000001704 04107 $$acze
000001704 046__ $$k2007-05-14
000001704 100__ $$aRozehnal, D.
000001704 24500 $$aNONSTACIONARY MEASUREMENT OF THE AIRFOIL AERODYNAMIC CHARACTERISTICS

000001704 24630 $$n13$$pEngineering Mechanics 2007
000001704 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Prague
000001704 506__ $$arestricted
000001704 520__ $$2eng$$aThis paper describes nonstacionary measurement of the airfoil aerodynamic characteristics at low speed wind tunnel on the University of Defence Brno. First part introduces the results for the airfoil in range of the angle of attack 0-360° with variable angle velocity. Further research focuses on experiments with high changes of the angle of attack with oscilations and variable frequences and amplitudes of motion.

000001704 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000001704 653__ $$a

000001704 7112_ $$aEngineering Mechanics 2007$$cSvratka (CZ)$$d2007-05-14 / 2007-05-17$$gEM2007
000001704 720__ $$aRozehnal, D.
000001704 8560_ $$ffischerc@itam.cas.cz
000001704 8564_ $$s914678$$uhttps://invenio.itam.cas.cz/record/1704/files/119-Rozehnal-PT.pdf$$y
             Original version of the author's contribution as presented on CD, .
            
000001704 962__ $$r1585
000001704 980__ $$aPAPER