Acoustic and flow characteristics of an airfoil fitted with morphed trailing edges
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DOI: 10.1016/j.expthermflusci.2020.110287
Abstract: Abstract An experimental study of a simple NACA 0012 airfoil fitted with two different flap profiles was carried out to characterize their aerodynamic and aeroacoustic performance. The airfoil with a flap deflection angle of β… read more here.
Keywords: morphed flap; flap airfoil; airfoil fitted; angles attack ... See more keywords