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Test Cases for Modeling and Validation of Structures with Piezoelectric ActuatorsA set of benchmark test articles were developed to validate techniques for modeling structures containing piezoelectric actuators using commercially available finite element analysis packages. The paper presents the development, modeling, and testing of two structures: an aluminum plate with surface mounted patch actuators and a composite box beam with surface mounted actuators. Three approaches for modeling structures containing piezoelectric actuators using the commercially available packages: MSC/NASTRAN and ANSYS are presented. The approaches, applications, and limitations are discussed. Data for both test articles are compared in terms of frequency response functions from deflection and strain data to input voltage to the actuator. Frequency response function results using the three different analysis approaches provided comparable test/analysis results. It is shown that global versus local behavior of the analytical model and test article must be considered when comparing different approaches. Also, improper bonding of actuators greatly reduces the electrical to mechanical effectiveness of the actuators producing anti-resonance errors.
Document ID
20010059241
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Reaves, Mercedes C.
(NASA Langley Research Center Hampton, VA United States)
Horta, Lucas G.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA Paper 2001-1466
Meeting Information
Meeting: 42nd AIAA/ASME/ASCE/AHS/ASC Structure and Structural Dynamics Conference
Location: Seattle, WA
Country: United States
Start Date: April 16, 2001
End Date: April 19, 2001
Sponsors: American Society of Mechanical Engineers, American Society for Composites, American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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