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DTIC ADA216226: A Study of Failure Characteristics in Thermoplastic...
by Defense Technical Information Center
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The purpose of this thesis was to determine (both
experimentally and analytically) the initiation and
progression of failure, stress-strain response, and the
failure loads of Graphite/Polyetheretherketone (Gr/PEEK)
laminates, incorporating an eccentric 0.4 inch circular
discontinuity, loaded in axial tension at room
temperature. For each ply lay-up, three values of
eccentricity were considered (the three values of
eccentricity were determined by the hole location within
each specimen). In addition, experimentation was
conducted to study the effects of boundary conditions on
the failure characteristics of the Gr/PEEK laminates;
this was accomplished through the use of a special
mounting fixture which allowed in-plane rotation of the
specimens. Finally, experimentation was conducted, using
photoelasticity, to verify the gross stress states of the
Gr/PEEK laminates predicted by the analytical study.
Analytically, a nonlinear material finite element program
was used to predict the initiation and progression of
failure, stress-strain response, and the failure loads of
the Gr/Peek laminates. In addition, the effects of
boundary conditions on the failure modes of the Gr/Peek
laminates was studied analytically. And finally, the
gross stress states of the Gr/PEEK laminates were
considered in the analytical portion of this thesis.
Date Published: 2018-02-24 00:50:34
Identifier: DTIC_ADA216226
Item Size: 98191984
Language: english
Media Type: texts
# Topics
DTIC Archive; Daniels, John A ; AIR F...
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