Experimental investigation on noise emissions of an airfoil with non-flat plate trailing edge serrations
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DOI: 10.1007/s12206-019-0601-x
Abstract: This paper presents an experimental study on the aeroacoustic characteristics of a NACA 0018 with nonflat plate-type serrated trailing edge at Reynolds numbers of 500000 in an open-jet wind tunnel. The experimental results show that… read more here.
Keywords: trailing edge; serrated trailing; experimental investigation; noise ... See more keywords