NASA NTRS · 19860029131
A damage tolerant design parameter for graphite/epoxy laminated composites
Abstract
The results of an extensive experimental investigation of the fracture behavior of notched graphite/epoxy laminates are presented. Twenty-seven laminates with different stacking sequences and laminate thicknesses have been studied. The data presented herein suggest that a damage tolerant design parameter exists that is relatively independent of ply stacking sequence and laminate thickness.
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Harris, C. E., Morris, D. H.. 1985-01-01. A damage tolerant design parameter for graphite/epoxy laminated composites. https://ntrs.nasa.gov/citations/19860029131
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