Progressive failure modeling in notched cross-ply fibrous composites
by Linda E. Craugh
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The objective of this study was to model and simulate progressive failure initiating from a notch tip in a laminated fibrous composite subjected to tensile in-plane loading. The micro/macro-level approach was used for this study. The micro-level analysis used the 3-D unit cell model while macro-level analysis used the finite element analysis technique. A cross-ply laminate with double-edge notches was studied to investigate delamination, fiber splitting, and transverse matrix cracking in the structure. Numerical results were compared to previous experimental work.
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Progressive failure modeling in notched cross-ply fibrous composites
1999, Naval Postgraduate School, Available from National Technical Information Service
in English
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Edition Notes
Thesis advisor(s): Young W. Kwon.
"March 1999".
Thesis (M.S. in Mechanical Engineering) Naval Postgraduate School, March 1999.
Includes bibliographical references (p. 47-48).
Approved for public release; distribution unlimited.
Also available online.
Mode of access: World Wide Web.
System requirements: Adobe Acrobat Reader 7.0.
US Navy (USN) author.
dk/dk cc:9116 5/20/99.
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