SEDL / STP / STP813-EB / STP31816S



Effects of Stress Ratio, Frequency, and Loading Time on the Tensile Fatigue of Glass-Reinforced Epoxy

Mandell, JF
Research associate, Massachusetts Institute of Technology, Cambridge, MA

Meier, U
Swiss Federal Laboratories for Testing Materials and Research, Dübendorf,


Pages: 23    Published: Jan 1983


Download this paper for $25 PDF (476K)          View License Agreement
Abstract

The interaction of time under load and number of tensile fatigue cycles has been investigated for 0°/90° E-glass/epoxy laminates. The frequency was varied from 0.01 to 1.0 Hz, and the stress ratio was varied from 0 to 1.0 (static fatigue). Square wave and spike loading data indicate a higher initial strength but also a higher rate of loss of initial strength per decade of cycles for waveforms with less time at maximum stress. S-N curves tend to converge at low stress to the same number of cycles to failure, regardless of waveform. Long-term results are reported for fiberglass box beams fatigued for up to 108 cycles at relatively low loads, where matrix cracking and delamination damage were studied. A brief description is also given of field failures involving crack growth in a brittle mode, normal to the fibers.


Keywords:
composite materials, glass epoxy, material fatigue, time dependence, tension, box beam, field failures, composites

Paper ID: STP31816S
Committee/Subcommittee: D30.02
DOI: 10.1520/STP31816S
CrossRef ASTM International is a member of CrossRef.