NASA NTRS · 20040085973
Fatigue Life Methodology for Bonded Composite Skin/Stringer Configurations
Abstract
A methodology is presented for determining the fatigue life of bonded composite skin/stringer structures based on delamination fatigue characterization data and geometric nonlinear finite element analyses. Results were compared to fatigue tests on stringer flange/skin specimens to verify the approach.
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Krueger, Ronald, Paris, Isabelle L., OBrien, T. Kevin. 2000-01-01. Fatigue Life Methodology for Bonded Composite Skin/Stringer Configurations. https://ntrs.nasa.gov/citations/20040085973
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