Finite element analysis of bonded patch repair of a panel with multiple cracks-Reference-Cited by-同舟云学术

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Finite element analysis of bonded patch repair of a panel with multiple cracks

Published:2020 Issue: Volume: Page:
ISSN:0094-243X
Container-title:AIP Conference Proceedings
language:
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Author:

Srilakshmi R.,Rao M. Vedanth,Kumar R. Sanjay

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5141595

Reference16 articles.

1. N. Duong and C. H. Wang. “Composite Repair - Theory and Design. 1st edition” (Elsevier Science and Technology publications 2007) pp 250–340.

2. Baker, L. R. F. Rose and R. Jones. “Advances in the Bonded Composite Repair of Metallic Aircraft Structure. 2nd edition”(Elsevier Science and Technology publications 2002), pp 320–345.

3. Optimum design of symmetric composite patch repair to centre cracked metallic sheet

4. Design, analysis and performance of adhesively bonded composite patch repair of cracked aluminum aircraft panels

5. Mixed-mode fracture analysis of aluminium repaired panels using composite patches

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1. Residual stress determination by blind hole drilling and local displacement mapping in aluminium alloy aerospace components;Frattura ed Integrità Strutturale;2024-05-25

2. Numerical analysis of sandwich panels under high-velocity impact;IOP Conference Series: Materials Science and Engineering;2022-07-01

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