000009195 001__ 9195
000009195 005__ 20141204092417.0
000009195 04107 $$aeng
000009195 046__ $$k12/05/2014
000009195 100__ $$aRozehnal, D.
000009195 24500 $$aUnsteady measurements of aerodynamic characteristics of the airfoil

000009195 24630 $$n18.$$pEngineering Mechanics 2012
000009195 260__ $$bInstitute of Theoretical and Applied Mechanics, AS CR, Prague
000009195 506__ $$arestricted
000009195 520__ $$2eng$$aThis paper deals with unsteady measurements of aerodynamic characteristics of the symmetric airfoil for the angle of attack within the range from 0° to 360° with variable value of angular velocity. These results are processed for first and second revolution of airfoil NACA 0012 Mod. A special device was designed for these tests.

000009195 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000009195 653__ $$aunsteady aerodynamic, dynamic stall, measurement, wind tunnel tests

000009195 7112_ $$aEngineering Mechanics 2012$$cSvratka (CZ)$$d12/05/2014 - 15/05/2014$$gEM2012
000009195 720__ $$aRozehnal, D.
000009195 8560_ $$ffischerc@itam.cas.cz
000009195 8564_ $$s505080$$uhttps://invenio.itam.cas.cz/record/9195/files/109_Rozehnal_D-FT.pdf$$yOriginal version of the author's contribution as presented on CD, paper (No. 109).
000009195 962__ $$r8924
000009195 980__ $$aPAPER