Layerwise Dynamic Response Models for Delamination Composite Beams with Active Piezoelectric Sensors
Author:
Affiliation:
1. Univ. of Patras
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2186
Reference28 articles.
1. Effect of Delamination on the Natural Frequencies of Composite Laminates
2. Detection of Debonding Damage in a Composite Plate through Natural Frequency Variations
3. Free vibrations of delaminated beams
4. Vibration of delaminated composite plates and some applications to non-destructive testing
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1. Analysis of Intact/Delaminated Composite and Sandwich Beams Using a Higher-Order Modeling Technique;Journal of Composites Science;2024-05-10
2. An extended layerwise spectral finite element framework for delamination growth simulation in laminated composite strips;Composite Structures;2021-11
3. Layerwise Theories of Laminated Composite Structures and Their Applications: A Review;Archives of Computational Methods in Engineering;2020-01-07
4. High Frequency Response of Delaminated Composite Beams with Active Piezoelectric Sensors;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07
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