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Simulation of Complex Cracking in Plain Weave C/SiC Composite under Biaxial LoadingFinite element analysis is performed on a mesh, based on computed geometry of a plain weave C/SiC composite with assumed internal stacking, to reveal the pattern of internal damage due to biaxial normal cyclic loading. The simulation encompasses intertow matrix cracking, matrix cracking inside the tows, and separation at the tow-intertow matrix and tow-tow interfaces. All these dissipative behaviors are represented by traction-separation cohesive laws. Not aimed at quantitatively predicting the overall stress-strain relation, the simulation, however, does not take the actual process of fiber debonding into account. The fiber tows are represented by a simple rule-of-mixture model where the reinforcing phase is a hypothetical one-dimensional material. Numerical results indicate that for the plain weave C/SiC composite, 1) matrix-crack initiation sites are primarily determined by large intertow matrix voids and interlayer tow-tow contacts, 2) the pattern of internal damage strongly depends on the loading path and initial stress, 3) compressive loading inflicts virtually no damage evolution. KEY WORDS: ceramic matrix composite, plain weave, cohesive model, brittle failure, smeared crack model, progressive damage, meso-mechanical analysis, finite element.
Document ID
20120016711
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cheng, Ron-Bin
(Dassault Systemes Simulia Corp. Warwick, RI, United States)
Hsu, Su-Yuen
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 26, 2013
Publication Date
October 1, 2012
Subject Category
Composite Materials
Report/Patent Number
NF1676L-14243
Report Number: NF1676L-14243
Meeting Information
Meeting: 27th Technical Conference
Location: Arlington, VA
Country: United States
Start Date: October 1, 2012
End Date: October 3, 2012
Funding Number(s)
WBS: WBS 984754.02.07.07.16.03.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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