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ASTM Selected Technical Papers
Nondestructive Evaluation and Flaw Criticality for Composite Materials
By
RB Pipes
RB Pipes
1
University of Delaware
,
editor
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WR Scott
WR Scott
2
University of Delaware
,
coeditor
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SV Kulkarni
SV Kulkarni
3
University of Delaware
,
coeditor
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WW Stinchcomb
WW Stinchcomb
4
University of Delaware
,
coeditor
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ISBN-10:
0-8031-0527-4
ISBN:
978-0-8031-0527-0
No. of Pages:
366
Publisher:
ASTM International
Publication date:
1979

The fracture surface morphologies of graphite/epoxy composite materials have been studied to determine the influences of load history, material configuration, temperature, moisture and matrix system type. Three commercially available systems with unidirectional tapes loaded in tension and fabrics tested in shear were chosen for analysis. Elevated temperature, moisture exposure, or both increase the amount of fiber pullout in the unidirectional tapes. Only in one case was the pullout fracture mode changed from a cohesive to an adhesive type of fracture process. The shear-loaded fabrics displayed either a tensile flexure fracture or an apparent shear fracture mode. The latter mode was believed to be actually a tensile rupture mode due to a resolution of shear stresses into tensile stresses. A transition temperature was defined to denote the temperature at which the fracture mode changed from tensile flexure to apparent shear. Significant differences in fracture surface morphology were observed among the three commercial graphite/epoxy systems.

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