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Micromechanics of fatigue in woven and stitched compositesThe goal is to determine how microstructural factors, especially the architecture of microstructural factors, control fatigue damage in 3D reinforced polymer composites. Test materials were fabricated from various preforms, including stitched quasi-isotropic laminates, and through-the-thickness angle interlock, layer-to-layer angle interlock, and through-the-thickness stitching effect weaves. Preforms were impregnated with a tough resin by a special vacuum infiltration method. Most tests are being performed in uniaxial compression/compression loading. In all cases to date, failure has occurred not by delamination, but by shear failure, which occurs suddenly rather than by gradual macroscopic crack growth. Some theoretical aspects of bridging are also examined.
Document ID
19930021661
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cox, B. N.
(Rockwell International Science Center Thousand Oaks, CA, United States)
Dadkhah, M. S.
(Rockwell International Science Center Thousand Oaks, CA, United States)
Inman, R. V.
(Rockwell International Science Center Thousand Oaks, CA, United States)
Mitchell, M. R.
(Rockwell International Science Center Thousand Oaks, CA, United States)
Morris, W. L.
(Rockwell International Science Center Thousand Oaks, CA, United States)
Schroeder, S.
(Rockwell International Science Center Thousand Oaks, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA. Langley Research Center, First NASA Advanced Composites Technology Conference, Part 2
Subject Category
Composite Materials
Accession Number
93N30850
Funding Number(s)
CONTRACT_GRANT: NAS1-18840
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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