Jan Wojciechowski, Tomasz Szuster, Jozef Pietrucha
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引用次数: 3
Abstract
A segment of the upper surface of a laminar airfoil model is submitted to forced vibrations at controlled frequency by means of piezo-electric actuators. The experiment carried out in a wind tunnel demonstrated an appreciable diminution of the profile drag for some ranges of the angle of attack and Reynolds number.
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