Strain energy release rate determination of prescribed cracks in adhesively-bonded single-lap composite joints with thick bondlines-Reference-Cited by-同舟云学术

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Strain energy release rate determination of prescribed cracks in adhesively-bonded single-lap composite joints with thick bondlines

Published:2008-07 Issue:5 Volume:39 Page:863-873
ISSN:1359-8368
Container-title:Composites Part B: Engineering
language:en
Short-container-title:Composites Part B: Engineering

Author:

Yang Chihdar,Chadegani Alireza,Tomblin John S.

Publisher

Elsevier BV

Subject

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

Reference30 articles.

1. Tomblin JS, Yang C, Harter P. Investigation of thick bondline adhesive joints. FAA Technical Report, DOT/FAA/AR-01/33; June 2001.

2. Yang C, Tomblin JS, Guan Z. Analytical modeling of ASTM lap shear adhesive specimens. FAA Technical Report, DOT/FAA/AR-02/130; February 2003.

3. Kutscha D. Mechanics of adhesive-bonded lap-type joints: survey and review. Technical Report AFML-TDR-64-298; 1964.

4. Kutscha D, Hofer KE, Jr. Feasibility of joining advanced composite flight vehicles. Technical Report AFML-TR-68-391; 1969.

5. A review of the strength of joints in fibre-reinforced plastics: Part 2 adhesively bonded joints;Matthews;Composites,1982

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