Parametric study on static and fatigue strength recovery of scarf-patch-repaired composite laminates-Reference-Cited by-同舟云学术

Parametric study on static and fatigue strength recovery of scarf-patch-repaired composite laminates

Published:2016-04 Issue: Volume:140 Page:417-432
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Yoo Jae-Seung,Truong Viet-Hoai,Park Min-Young,Choi Jin-Ho,Kweon Jin-Hwe

Funder

Ministry of Trade, Industry and Energy

Agency for Defense Development

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference21 articles.

1. Defects and damage in composite materials and structures;Heslehurst,2014

2. Federal Aviation Administration. Dept. of transportation, Bonded repair of aircraft composite sandwich structures. DOT/FAA/AR-03/74, Washington, DC; 2004.

3. Improved design methods for scarf repairs to highly strained composite aircraft structure;Harman;Compos Struct,2006

4. Composite materials for aircraft structures;Baker,2004

5. Modelling single and double-lap repairs on composite materials;Campilho;Composite,2005

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