Airfoil trailing-edge noise and drag reduction at a moderate Reynolds number using wavy geometries
نویسندگان
چکیده
This study utilizes a hybrid aeroacoustic model to investigate how airfoils with spanwise wavy geometries can be used reduce trailing-edge noise alongside improving the aerodynamic performance. A smooth airfoil is compared four variants, which have surface waves of different wavelengths, at Reynolds number Re = 64 000 and an angle-of-attack 1°. The first three variants geometry modified by single wavelength, whereas fourth has composed two creates more irregular variation. results show that modest reductions around 4 dB are achieved for but much larger reduction 17.7 variant. mechanisms behind explored, it shown reduces correlation pressure fluctuations also modifies boundary layer dynamics, contributes large reduction. It further drag force reducing shear stress over parts limiting flow separation on suction side. variant assessed across wider range angles ([Formula: see text]) produce less than wing entire as well [Formula: text].
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ژورنال
عنوان ژورنال: Physics of Fluids
سال: 2022
ISSN: ['1527-2435', '1089-7666', '1070-6631']
DOI: https://doi.org/10.1063/5.0120124