Impact damage tolerance of composite repairs to highly-loaded, high temperature composite structures-Reference-Cited by-同舟云学术

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Impact damage tolerance of composite repairs to highly-loaded, high temperature composite structures

Published:2011-10 Issue:10 Volume:42 Page:1321-1334
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:

Harman A.B.,Rider A.N.

Publisher

Elsevier BV

Subject

Mechanics of Materials,Ceramics and Composites

Reference11 articles.

1. A theory of adhesive scarf joints;Lubkin;J Appl Mech,1957

2. Hart Smith J. Adhesive-bonded scarf and stepped-lap joints. McDonnell-Douglas Corporation; 1973.

3. Scarf repairs to highly strained graphite/epoxy structure;Baker;Int J Adhes Adhes,1999

4. Harman A. Optimisation and improvement of the design of scarf repairs to aircraft. University of New South Wales; 2006.

5. On the design methodology of scarf repairs to composite laminates;Gunnion;Compos Sci Technol,2007

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1. An experimental investigation of tensile residual strength of repaired composite laminates after low velocity impact;Thin-Walled Structures;2024-07

2. Fatigue life simulation of the impacted carbon/epoxy composite laminates;Composites Part A: Applied Science and Manufacturing;2024-06

3. Study on the low‐velocity impact response of the repaired carbon fiber‐reinforced plastic laminates: Bonded versus scarf repair;Polymer Composites;2024-01-12

4. Tension-after-impact (TAI) performance and 3D damage visualization of carbon-fiber epoxy composites with adhesively bonded patch repairs;Composite Structures;2023-10

5. Experimental Study on Impact Damage Resistance and Residual Compression Behaviors of Scarf Repaired Composite Plates;Applied Composite Materials;2023-04-11

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