Skip to Main Content
Skip Nav Destination
ASTM Selected Technical Papers
Fractography of Modern Engineering Materials: Composites and Metals
By
JE Masters
JE Masters
1
Senior Research Engineer
,
American Cyanamid Co.
,
Stamford, CT 06904
;
symposium cochairman and coeditor
.
Search for other works by this author on:
JJ Au
JJ Au
2
Sundstrand Corp.
,
editor
Search for other works by this author on:
ISBN-10:
0-8031-0950-4
ISBN:
978-0-8031-0950-6
No. of Pages:
470
Publisher:
ASTM International
Publication date:
1987

A series of angleplied graphite/epoxy laminates was fabricated from overaged prepreg and tested in tension to investigate the effects of overaged or “advanced-cure” material on the degradation of laminate strength. Results which include fracture stresses indicate a severe degradation in strength. In addition, the fracture surfaces and microstructural characteristics are distinctly unlike any features observed in previous tests of this prepreg and laminate configuration. Photographs of the surface and microstructures reveal flat morphologies consisting of alternate rows of fibers and hackles. These fracture surface characteristics are independent of the laminate configurations. The photomicrographs are presented and compared with data from similar studies to show the unique characteristics produced by the overaged prepreg. Analytical studies produced results which agreed with those from the experimental investigations.

1.
Irvine
,
T. B.
and
Ginty
,
C. A.
, “
Progressive Fracture of Fiber Composites
,” NASA TM-83701,
National Aeronautics and Space Administration
,
Washington, DC
,
1983
.
2.
Ginty
,
C. A.
and
Irvine
,
T. B.
, “
Fracture Surface Characteristics of Notched Angleplied Graphite/Epoxy Composites
,” NASA TM-83786,
National Aeronautics and Space Administration
,
Washington, DC
,
1984
.
3.
Irvine
,
T. B.
and
Ginty
,
C. A.
, “
Fracture Modes in Notched Angleplied Composite Laminates
,” NASA TM-83802,
National Aeronautics and Space Administration
,
Washington, DC
,
1984
.
4.
Clements
,
L. L.
, “
Deformation and Failure Mechanisms of Graphite/Epoxy Composites Under Static Loading
,” (FR-22-3,
Advanced Research and Applications Corp.
, NASA Contract NAS 2-9989),
Clements
,
L. L.
, “
Deformation and Failure Mechanisms of Graphite/Epoxy Composites Under Static Loading
,” NASA CR-166328,
National Aeronautics and Space Administration
,
Washington, DC
,
1981
.
5.
Clements
,
L. L.
and
Adamson
,
M. J.
, “
Failure of Morphology of (0°)8 Graphite/Epoxy as Influenced by Environments and Processing
,” NASA TM-81318,
National Aeronautics and Space Administration
,
Washington, DC
,
1981
.
6.
Murthy
,
P. L. N.
and
Chamis
,
C. C.
, “
ICAN: Integrated Composites Analyzer
,” AIAA Paper 84-0974,
American Institute of Aeronautics and Astronautics
,
New York
,
05
1984
.
This content is only available via PDF.
You do not currently have access to this chapter.
Close Modal

or Create an Account

Close Modal
Close Modal