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Published in 2017 at "Journal of Composite Materials"
DOI: 10.1177/0021998316669579
Abstract: Finite element simulations of three laminates in open-hole configuration subjected to constant amplitude tension–tension fatigue loading are investigated as part of the Damage Tolerant Design Principles program organized by the Air Force Research Laboratory. All…
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Keywords:
fatigue loading;
fatigue;
im7 977;
autodesk helius ... See more keywords