Towards a practical structural health monitoring technology for patched cracks in aircraft structure-Reference-Cited by-同舟云学术

Towards a practical structural health monitoring technology for patched cracks in aircraft structure

Published:2009-09 Issue:9 Volume:40 Page:1340-1352
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

Baker Alan,Rajic Nik,Davis Claire

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference16 articles.

1. Advances in the bonded composite repair of aircraft structure,2002

2. IBID Reference 1, Baker AA, Chapter 22, Certification Issues for Critical Repairs.

3. IBID Reference 1, Roach DP, Scala CM, Chapter 23, Non-destructive Evaluation and Quality Control for Bonded Composite Repair of Metallic Aircraft Structures.

4. IBID Reference 1, Galea SC, Chapter 20, Smart Patch Systems.

5. The development of a boron/epoxy doubler system for the F-111 wing pivot fitting – materials engineering aspects;Baker;Composites,1993

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