Failure Behavior of Composite Laminates with Multi-Pin Loaded Holes
Source abstract
Abstract
The aim of this study is to determine the failure behavior of laminated glass—epoxy composite plate which is subjected to a traction force by four pins. The failure load and failure mode of composite plates which have the stacking sequence of [0/90/±45] S has been observed experimentally. The ratio of edge distance from the hole center to pin diameter (E/D), the ratio of longitudinal holes distance to pin diameter (F/D) and the ratio of transverse holes distance to pin diameter (G/D) were selected as parameters. The results showed that the specimens except for E/D = 2 have similar behavior in terms of failure loads and failure modes.
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Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Analysis of Composite Materials · Composite Structure Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Department of Mechanical Engineering, Dokuz Eylül University 35100, Izmir, Turkey,
Department of Mechanical Engineering, Dokuz Eylül University 35100, Izmir, Turkey
Turkish Aerospace Industries (TAI), Inc., 06980, Ankara, Turkey
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