NASA NTRS · 19880013561
Fatigue damage development of various CFRP-laminates
Abstract
The chronic strength and fatigue behavior of a woven carbon-fiber reinforced laminate in a balanced eight-shaft satin weave style was compared to nonwoven laminates with an equivalent cross-ply layup. Half the fibers were arranged in the direction of the load and the other half perpendicular to it. Two types of nonwoven laminates consisting of continuous fibers and aligned discontinuous fibers, both produced from carbon fiber prepregs, were studied. The cross-ply laminate with continuous fiber showed the best characteristics with regard to both static strength and fatigue. The similarities and differences in damage mechanisms in the laminates are described.
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Schulte, K., Baron, CH.. 1988-05-01. Fatigue damage development of various CFRP-laminates. https://ntrs.nasa.gov/citations/19880013561
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