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 Google Scholar
Right arrow Citing Articles via Scopus
Google Scholar
Right arrow Articles by Lissenden, C. J.
Right arrow Articles by Pindera, M. J.
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?

Response of SiC/Ti under Combined Loading Part II: Room Temperature Creep Effects

C. J. Lissenden

Department of Engineering Mechanics, University of Kentucky, Lexington, KY 40506-0046

C. T. Herakovich

Department of Civil Engineering and Applied Mechanics, University of Virginia, Charlottesville, VA 22903-2442

M. J. Pindera

Department of Civil Engineering and Applied Mechanics, University of Virginia, Charlottesville, VA 22903-2442

Results from cyclic multiaxial tests on [±45], silicon carbide/titanium (SiC/Ti) tubular specimens at room temperature are presented. One test cycle consisted of applying axial stress at a constant rate, holding the axial stress constant at a predetermined level for a fixed period of time, applying shear stress at a constant rate, holding the shear stress constant at a predetermined level for a fixed period of time, unloading the shear stress, and finally, unloading the axial stress. Test results show that relatively large axial time dependent, and to a lesser extent, time independent strains are accumulated after the axial stress is held constant. The time dependent accumulated axial strains are termed creep, while the time independent strains are due to coupling between shear and axial strain. The results of short duration creep tests conducted on a bulk titanium alloy (Ti-15-3) are also presented and are consistent with the results from the multiaxial tests on SiC/Ti

Key Words: titanium matrix composites • multiaxial loading • damage evolution • strain accumulation • time dependent response • shear coupling • acoustic emissions

Journal of Composite Materials, Vol. 29, No. 10, 1403-1417 (1995)
DOI: 10.1177/002199839502901008


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?