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High-Fidelity Modeling for Health Monitoring in Honeycomb Sandwich StructuresHigh-Fidelity Model of the sandwich composite structure with real geometry is reported. The model includes two composite facesheets, honeycomb core, piezoelectric actuator/sensors, adhesive layers, and the impactor. The novel feature of the model is that it includes modeling of the impact and wave propagation in the structure before and after the impact. Results of modeling of the wave propagation, impact, and damage detection in sandwich honeycomb plates using piezoelectric actuator/sensor scheme are reported. The results of the simulations are compared with the experimental results. It is shown that the model is suitable for analysis of the physics of failure due to the impact and for testing structural health monitoring schemes based on guided wave propagation.
Document ID
20110014302
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Luchinsky, Dimitry G.
(Mission Critical Technologies, Inc. Moffett Field, CA, United States)
Hafiychuk, Vasyl
(SGT, Inc. Greenbelt , MD, United States)
Smelyanskiy, Vadim
(NASA Ames Research Center Moffett Field, CA, United States)
Tyson, Richard W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Walker, James L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Miller, Jimmy L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
March 5, 2011
Subject Category
Composite Materials
Report/Patent Number
ARC-E-DAA-TN3100
Report Number: ARC-E-DAA-TN3100
Meeting Information
Meeting: 2011 IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 5, 2011
End Date: March 12, 2011
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
PROJECT: Project No. 00219.001.095.003
CONTRACT_GRANT: NNM05AA22A
CONTRACT_GRANT: NNA08CG83C
Distribution Limits
Public
Copyright
Public Use Permitted.
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