Online Guided Wave-Based Debonding Detection in Honeycomb Sandwich Structures
Author:
Affiliation:
1. University of Arkansas at Little Rock, Little Rock, Arkansas 72204
2. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050891
Reference34 articles.
1. Effective Thermal/Mechanical Properties of Honeycomb Core Panels for Hot Structure Applications
2. Predicting delamination and debonding in modern aerospace composite structures
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