Stress Analysis of Bonded Patched Plates with Circular Cutout Using Full-Discrete Layer Model
Author:
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering
Link
http://www.tandfonline.com/doi/pdf/10.1080/15376494.2012.699592
Reference25 articles.
1. Repair of cracked or defective metallic aircraft components with advanced fibre composites—an overview of Australian work
2. Fibre composite repair of cracked metallic aircraft components — practical and basic aspects
3. Effects of adherend deflections in single lap joints
4. An evaluation of analytical and numerical solutions to the single-lap joint
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