Return to search

Stiffness reduction resulting from transverse cracking in fiber- reinforced composite laminates

Several damage modes, including fiber breakage, delamination, and transverse cracking, have been observed to contribute to the mechanical degradation of fiber-reinforced composite laminates. In this investigation, the effect of transverse cracking on laminate stiffness was studied. Four. glass-epoxy laminates ([0,90₃]<sub>s</sub>, [90₃,0]<sub>s</sub>, [0,90]<sub>s</sub>, and [0,±45]<sub>s</sub>) were evaluated.

Two experimental test sequences were performed. In the first test sequence, longitudinal stiffness was measured at various stages of damage development. Damage development was monitored via edge replication. In the second test sequence, four laminate stiffnesses (E<sub>xx</sub>, v<sub>xy</sub>, G<sub>xy</sub>, and D<sub>yy</sub>) were measured in the undamaged and near-saturation damage states.

Two analytical models were evaluated. A one dimensional shear lag model was used to predict longitudinal stiffness as a function of crack density for the [0,90₃]<sub>s</sub> and 90₃,0]<sub>s</sub> laminates. Correlation between theory and experiment was good. A modified laminate analysis was used to predict four laminate stiffnesses (E<sub>xx</sub>, v<sub>xy</sub>, G<sub>xy</sub>, and D<sub>yy</sub>). Except for the [0,±45]<sub>s</sub> case, a laminate in which significant amounts of damage - s other than transverse cracking were observed, agreement between pre- · dieted and observed stiffness changes was good. / Master of Science

Identiferoai:union.ndltd.org:VTETD/oai:vtechworks.lib.vt.edu:10919/71009
Date January 1981
CreatorsHighsmith, Alton L.
ContributorsEngineering Mechanics
PublisherVirginia Polytechnic Institute and State University
Source SetsVirginia Tech Theses and Dissertation
Languageen_US
Detected LanguageEnglish
TypeThesis, Text
Formatvii, 90, [1] leaves, application/pdf, application/pdf
RightsIn Copyright, http://rightsstatements.org/vocab/InC/1.0/
RelationOCLC# 8016205

Page generated in 0.0018 seconds