A simple method for determining the effects of bolt–hole clearance on load distribution in single-column multi-bolt composite joints-Reference-Cited by-同舟云学术

A simple method for determining the effects of bolt–hole clearance on load distribution in single-column multi-bolt composite joints

Published:2006-05 Issue:1 Volume:73 Page:78-87
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

McCarthy M.A.,McCarthy C.T.,Padhi G.S.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference9 articles.

1. Tate MB, Rosenfeld SJ. Preliminary investigation of the loads carried by individual bolts in bolted joints. NACA TN 1051, May 1946.

2. Nelson WD, Bunin BL, Hart-Smith LJ. Critical joints in large composite aircraft structure. NASA CR-3710, August 1983.

3. Load distribution of multi-fastener laminated composite joints;Fan;Int J Solids Struct,1993

4. McCarthy MA, Lawlor VP, Stanley WF. An experimental study of bolt–hole clearance effects in single-lap, multi-bolt composite joints. J Compos Mater, in press.

5. Bearing strength behaviour of clearance-fit fastener holes in toughened graphite/epoxy laminates;DiNicola,1993

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