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Finite element analysis of cracks in aging aircraft structures with bonded composite-patch repairs

  • Published:2011-04 Issue:3 Volume:42 Page:505-510
  • ISSN:1359-8368
  • Container-title:Composites Part B: Engineering
  • language:en
  • Short-container-title:Composites Part B: Engineering

Author:

Gu Linxia,Kasavajhala Ananth Ram Mahanth,Zhao Shijia

Funder

National Science Foundation

National Aeronautics and Space Administration

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference26 articles.

1. Repair of cracked or defective metallic components with advanced fiber composites an overview of Australian work;Baker;Compos Struct,1984

2. Principles of composite material mechanics;Gibson,1994

3. Determination of SIF for patched crack in aluminum plates by the combined finite element and genetic algorithm approach;Ergun;Fatigue Fract Eng Mater Struct,2008

4. Full-width disbonding effect on the repaired cracks in structural panels with bonded composite patches;Ouinas;J Thermoplast Compos Mater,2009

5. Analytical and finite element comparisons of stress intensity factors of composite materials;Dirikolu;Compos Struct,2000

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