28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-3.11.1

AIRFOIL SELF NOISE REDUCTION BY APPLICATION OF DIFFERENT TYPES OF TRAILING EDGE SERRATIONS

F. M. Catalano, L. D. Santana
Univ. of São Paulo, Brazil

Keywords: serrated trailing edge, noise reduction

This work presents an experimental study the effect of adding three different geometries of trailing-edge serrations, to a two-dimensional NACA 0012. The wing model has 92 pressure tapings for aerodynamic analisys which was complemented with trailing edge boundary layer measurements and wake mapping using hot wire measurements

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