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August 1, 1998AIAA Journal209 citations

Use of Piezoelectric Actuators for Airfoil Separation Control

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ASAvi SeifertSES. EliahuDGDavid Greenblatt

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Abstract

Surface-mounted piezoelectric actuators are used to excite the turbulent boundary layer upstream of separation, where the actuators interact directly with the boundary layer. The actuators are rigid and do not attenuate with increased aerodynamic loading up to the maximum tested speed of 30 m/s

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Cite This Study

Seifert et al. (1998) studied this question.

synapsesocial.com/papers/69d8891fd2f7327e70ae3522https://doi.org/10.2514/2.549
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