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ASTM Selected Technical Papers
Composite Materials: Testing and Design (Seventh Conference)
By
JM Whitney
JM Whitney
1
Materials Research Engineer
,
Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base
,
OH
;
symposium chairman and editor
.
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ISBN-10:
0-8031-0447-2
ISBN:
978-0-8031-0447-1
No. of Pages:
467
Publisher:
ASTM International
Publication date:
1986

A detailed analysis of the dynamic stress field in smooth and notched fiber composite (Charpy-type) specimens is reported in this paper. The analysis is performed with the aid of the direct transient response analysis solution sequence of MSC/NASTRAN. Three unidirectional composites were chosen for the study. They are S-glass/epoxy, Kevlar/epoxy, and T-300/epoxy composite systems. The specimens are subjected to an impact load that is modeled as a triangular impulse with a maximum of 8960 N (2000 lb) and a duration of 1 ms. The results are compared with those of static analysis of the specimens subjected to a peak load of 8960 N (2000 lb). For the geometry and type of materials studied, the static analysis results gave close conservative estimates for the dynamic stresses.

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