0
TECHNICAL PAPERS

An Information System for Damage Tolerance of Polymer Matrix Composites

[+] Author and Article Information
Ozgur Turkgenc, Reza Dianati, Milan Mitrovic, H. Thomas Hahn

Mechanical & Aerospace Engineering Department, University of California, Los Angeles, CA 90095-1597

Peter Shyprykevich

FAA William J. Hughes Technical Center, AAR-430, Atlantic City Int’l Airport, NJ 08405

J. Eng. Mater. Technol 121(4), 524-529 (Oct 01, 1999) (6 pages) doi:10.1115/1.2812410 History: Received December 01, 1998; Revised May 21, 1999; Online November 27, 2007

Abstract

Much research has been conducted to understand the damage tolerance behavior of polymer matrix composites, but there are so many parameters involved that the development of a generic model is rather difficult. The present paper proposes an information system, which can overcome such difficulty. In this system, a list of possible parameters is generated and used as input. The output contains compression strength after impact, dent depth and damage area as well as pertinent reference information. The information system is constituted in a relational database environment and tools from expert system technology are incorporated. Case examples are included to demonstrate the practical use of the software for both data retrieval and similarity studies.

Copyright © 1999 by The American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.

References

Figures

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