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Design Optimization Tool for Synthetic Jet Actuators Using Lumped Element ModelingThe performance specifications of any actuator are quantified in terms of an exhaustive list of parameters such as bandwidth, output control authority, etc. Flow-control applications benefit from a known actuator frequency response function that relates the input voltage to the output property of interest (e.g., maximum velocity, volumetric flow rate, momentum flux, etc.). Clearly, the required performance metrics are application specific, and methods are needed to achieve the optimal design of these devices. Design and optimization studies have been conducted for piezoelectric cantilever-type flow control actuators, but the modeling issues are simpler compared to synthetic jets. Here, lumped element modeling (LEM) is combined with equivalent circuit representations to estimate the nonlinear dynamic response of a synthetic jet as a function of device dimensions, material properties, and external flow conditions. These models provide reasonable agreement between predicted and measured frequency response functions and thus are suitable for use as design tools. In this work, we have developed a Matlab-based design optimization tool for piezoelectric synthetic jet actuators based on the lumped element models mentioned above. Significant improvements were achieved by optimizing the piezoceramic diaphragm dimensions. Synthetic-jet actuators were fabricated and benchtop tested to fully document their behavior and validate a companion optimization effort. It is hoped that the tool developed from this investigation will assist in the design and deployment of these actuators.
Document ID
20050239565
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Gallas, Quentin
(Florida Univ. Gainesville, FL, United States)
Sheplak, Mark
(Florida Univ. Gainesville, FL, United States)
Cattafesta, Louis N., III
(Florida Univ. Gainesville, FL, United States)
Gorton, Susan A.
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
OTHER: 23-714-80-VC
CONTRACT_GRANT: NAG1-03031
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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