An experimental investigation of tip vortex flow from a NACA0012 airfoil, pitched periodically at various frequencies, is conducted in a low-speed wind tunnel. Initially, data for stationary airfoil held fixed at various angles-of-attack are gathered. Flow visualization pictures as well as detailed cross-sectional properties areobtained at various streamwise locations using hot-wire anemometry. Data include mean velocity, streamwise vorticity as well as various turbulent stresses. Preliminary data are also acquired for periodically pitched airfoil. These results are briefly presented in this extended abstract.
Experimental Study of Tip Vortex Flow from a Periodically Pitched Airfoil Section
AIAA Aerospace Sciences Meeting (SciTech) ; 2016 ; San Diego, CA, United States
2016-01-04
Sonstige
Keine Angabe
Englisch
Experimental Study of Tip Vortex Flow from a Periodically Pitched Airfoil Section (AIAA 2016-1846)
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