Technical Paper

BOUNDARY ELEMENT MODELING FOR DELAMINATION ANALYSIS OF LAMINATED COMPOSITE STRUCTURES

VFS-F58-00023

6/11/2002

Event
Forum 58 - Montreal, Canada 2002
Authors
Andrew Makeev Delta Airlines
Erian A. Armanios Georgia Institute of Technology
Xin-Yuan Tan Georgia Institute of Technology
Samer Tawfik Georgia Institute of Technology
Abstract
Content

A simple 2D boundary element analysis, suitable for developing cost effective models for tapered composite laminates, is presented. Constant stress and displacement elements are used. Closed-form fundamental solutions are derived. Numerical results are provided for several configurations to illustrate the accuracy of the model.

Meta Tags
Topics
Simulation and modeling
Composite materials
Affiliated or Co-Author
Delta Airlines
Georgia Institute of Technology
Details
DOI
https://doi.org/10.4050/VFS-F58-00023
Citation
Makeev, A., Armanios, E., Tan, X., and Tawfik, S., "BOUNDARY ELEMENT MODELING FOR DELAMINATION ANALYSIS OF LAMINATED COMPOSITE STRUCTURES," Forum 58 - Montreal, Canada 2002, Montreal, Canada, June 11, 2002, https://doi.org/10.4050/VFS-F58-00023.
Additional Details
Publisher
The Vertical Flight Society
Published
6/11/2002
Product Code
VFS-F58-00023
Content Type
Technical Paper
Language
English