Advanced Search

Journal Navigation

Journal Home

Subscriptions

Archive

Contact Us

Table of Contents

SAGETRACK

Sign In to gain access to subscriptions and/or personal tools.
Journal of Reinforced Plastics and Composites
This Article
Right arrow Full Text (PDF)
Right arrow All Versions of this Article:
0731684407087744v1
28/9/1139    most recent
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 Google Scholar
Right arrow Citing Articles via Scopus
Google Scholar
Right arrow Articles by Noda, J.
Right arrow Articles by Miyano, Y.
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?

Statistical Scatter of Creep and Fatigue Failure Times for CFRP Laminates

Junji Noda

Graduate School of Science and Engineering, Yamaguchi University 2-16-1 Tokiwadai, Ube, Yamaguchi 755-8611, Japan, nodaj{at}yamaguchi-u.ac.jp

Masayuki Nakada

Materials System Research Laboratory, Kanazawa Institute of Technology 3-1 Yatsukaho, Hakusan, Ishikawa 924-0838, Japan

Yasushi Miyano

Materials System Research Laboratory, Kanazawa Institute of Technology 3-1 Yatsukaho, Hakusan, Ishikawa 924-0838, Japan

This article is concerned with the prediction of statistical scatter for the creep and fatigue failure times of CFRP laminates by using the statistical scatter of strength measured at constant strain rate tests (CSR strength) based on the kinetic crack growth law (Christensen and Miyano). First, the time- and temperature-dependent CSR strengths for CFRP laminates were measured at two levels of temperatures, room temperature and 120°C, in the vicinity of glass transition temperature, and the statistical scatter of these CSR strengths were determined at these two levels of temperature. Furthermore, the statistical scatters of the creep and fatigue failure times at an arbitrary load level and a constant frequency at these two levels of temperatures were predicted using the statistical scatters for CSR strengths based on the kinetic crack growth law. On the other hand, the creep and the fatigue failure times were experimentally measured at the same conditions. It was clear that the statistical scatter for creep and fatigue failure times of CFRP laminates can be predicted using those for CSR strengths from the agreement of the experimental results and the predicted ones.

Key Words: CFRP • viscoelasticity • creep • fatigue • failure time • scatter • statistics.

This version was published on May 1, 2009

Journal of Reinforced Plastics and Composites, Vol. 28, No. 9, 1139-1148 (2009)
DOI: 10.1177/0731684407087744


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?