Advanced Search

Journal Navigation

Journal Home

Subscriptions

Archive

Contact Us

Table of Contents

Sign In to gain access to subscriptions and/or personal tools.
Journal of Composite Materials
This Article
Right arrow Full Text (PDF)
Right arrow References
Right arrow Alert me when this article is cited
Right arrow Alert me if a correction is posted
Services
Right arrow Email this article to a friend
Right arrow Similar articles in this journal
Right arrow Alert me to new issues of the journal
Right arrow Add to Saved Citations
Right arrow Download to citation manager
Right arrowRequest Permissions
Right arrow Request Reprints
Right arrow Add to My Marked Citations
Citing Articles
Right arrow Citing Articles via HighWire
Right arrow Citing Articles via Google Scholar
Right arrow Citing Articles via Scopus
Google Scholar
Right arrow Articles by Coats, T. W.
Right arrow Articles by Harris, C. E.
Right arrow Search for Related Content
Social Bookmarking
 Add to CiteULike   Add to Complore   Add to Connotea   Add to Del.icio.us   Add to Digg   Add to Reddit   Add to Technorati   Add to Twitter  
What's this?

A Progressive Damage Methodology for Residual Strength Predictions of Notched Composite Panels

Timothy W. Coats

National Research Council

Charles E. Harris

NASA Langley Research Center, MS-121, Hampton, VA 23681-0001

The translaminate fracture behavior of carbon/epoxy structural laminates with through-penetration notches was investigated to develop a residual strength prediction methodology for composite structures. An experimental characterization of several composite materials systems revealed a fracture resistance behavior that resembles the R-curve behavior exhibited by ductile metals. Fractographic examinations led to the postulate that the damage growth resistance was primarily due to fractured fibers in the principal load-carrying plies being bridged by intact fibers of the adjacent plies. The load transfer associated with this bridging mechanism suggests that a progressive damage analysis methodology will be appropriate for predicting the residual strength of laminates with through-penetration notches. A progressive damage methodology developed by the authors was used to predict the initiation and growth of matrix cracks and fiber fracture. The residual strength predictions for different panel widths, notch lengths, and material systems were in reasonable agreement to the experimental failure loads.

Key Words: composites • damage • matrix cracks • fiber fracture • internal state variable • residual strength

Journal of Composite Materials, Vol. 33, No. 23, 2193-2224 (1999)
DOI: 10.1177/002199839903302303


Add to CiteULike CiteULike   Add to Complore Complore   Add to Connotea Connotea   Add to Del.icio.us Del.icio.us   Add to Digg Digg   Add to Reddit Reddit   Add to Technorati Technorati   Add to Twitter Twitter    What's this?


This article has been cited by other articles:


Home page
Journal of Composite MaterialsHome page
S. R. Hallett and M. R. Wisnom
Numerical Investigation of Progressive Damage and the Effect of Layup in Notched Tensile Tests
Journal of Composite Materials, July 1, 2006; 40(14): 1229 - 1245.
[Abstract] [PDF]


Home page
Journal of Composite MaterialsHome page
S. R. Hallett and M. R. Wisnom
Experimental Investigation of Progressive Damage and the Effect of Layup in Notched Tensile Tests
Journal of Composite Materials, January 1, 2006; 40(2): 119 - 141.
[Abstract] [PDF]