The NASA Macro-Fiber Composite actuator is a flexible piezoelectric composite device designed for controlling vibrations and shape deformations in high performance aerospace structures. A complete method for fabricating the standard NASA Macro-Fiber Composite actuator is presented in this document. When followed precisely, these procedures will yield devices with electromechanical properties identical to the standard actuator manufactured by NASA Langley Research Center.High, James W. and Wilkie, W. KeatsLangley Research CenterPIEZOELECTRIC ACTUATORS; FABRICATION; ELECTROMECHANICS; AIRCRAFT STRUCTURES; FIBER COMPOSITES; VIBRATION; SHAPES
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