0
TECHNICAL PAPERS

The Fiber Composite With Nonlinear Interface—Part II: Antiplane Shear

[+] Author and Article Information
A. J. Levy

Department of Mechanical, Aerospace and Manufacturing Engineering, Syracuse University, Syracuse, NY 13244-1240

J. Appl. Mech 67(4), 733-739 (Jun 25, 2000) (7 pages) doi:10.1115/1.1329320 History: Received May 07, 1999; Revised June 25, 2000
Copyright © 2000 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
Composite cylinder geometry
Grahic Jump Location
The tangential interface force law
Grahic Jump Location
Bounds on antiplane shear stress-strain response, c=0.5,ρ=0.01
Grahic Jump Location
Effect of force length ratio on antiplane shear stress-strain response, c=0.3
Grahic Jump Location
Effect of concentration on antiplane shear stress-strain response, ρ=0.01

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In