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Failure models for textile compositesThe goals of this investigation were to: (1) identify mechanisms of failure and determine how the architecture of reinforcing fibers in 3D woven composites controlled stiffness, strength, strain to failure, work of fracture, notch sensitivity, and fatigue life; and (2) to model composite stiffness, strength, and fatigue life. A total of 11 different angle and orthogonal interlock woven composites were examined. Composite properties depended on the weave architecture, the tow size, and the spatial distributions and strength of geometrical flaws. Simple models were developed for elastic properties, strength, and fatigue life. A more complicated stochastic model, called the 'Binary Model,' was developed for damage tolerance and ultimate failure. These 3D woven composites possessed an extraordinary combination of strength, damage tolerance, and notch insensitivity.
Document ID
19960009403
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cox, Brian
(Rockwell International Science Center Thousand Oaks, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-4686
NAS 1.26:4686
Report Number: NASA-CR-4686
Report Number: NAS 1.26:4686
Accession Number
96N16569
Funding Number(s)
PROJECT: RTOP 510-02-11-07
CONTRACT_GRANT: NAS1-19243
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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