NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fatigue Life Methodology for Bonded Composite Skin/Stringer ConfigurationsA 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.
Document ID
20040085973
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Krueger, Ronald
(National Academy of Sciences - National Research Council Hampton, VA, United States)
Paris, Isabelle L.
(National Academy of Sciences - National Research Council Hampton, VA, United States)
OBrien, T. Kevin
(Army Research Lab. Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2000
Publication Information
Publication: Proceedings of the American Society for Composites, Fifteenth Technical Conference
ISBN: 1-58716-053-6
Subject Category
Composite Materials
Meeting Information
Meeting: Fifteenth Technical Conference
Country: Unknown
Start Date: January 1, 2000
Sponsors: American Society for Composites
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available