Accession Number:

AD0725753

Title:

The Influence of Stacking Sequence on Laminate Strength.

Descriptive Note:

Technical rept. Sep-Nov 70,

Corporate Author:

AIR FORCE MATERIALS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1971-03-01

Pagination or Media Count:

21.0

Abstract:

Based upon considerations relating to the nature of the interlaminar stresses in composite laminates, an approach is presented to predict the detailed stacking sequence of specific layer orientations which leads to optimum protection against delamination under uniaxial static and fatigue loadings. It is argued that the interlaminar normal stress, as well as the interlaminar shear stress, is instrumental in precipatating delamination and subsequent strength degradation. Correlation with existing experimental evidence of the stacking sequence phenomenon is presented. Author-PL

Subject Categories:

  • Laminates and Composite Materials

Distribution Statement:

APPROVED FOR PUBLIC RELEASE