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Calculation of residual principal stresses in CVD boron on carbon filamentsA three-dimensional finite element model of the chemical vapor deposition of boron on a carbon substrate (B/C) is developed. The model includes an expansion of the boron after deposition due to atomic rearrangement and includes creep of the boron and carbon. Curves are presented showing the variation of the principal residual stresses and the filament elongation with the parameters defining deposition strain and creep. The calculated results are compared with experimental axial residual stress and elongation measurements made on B/C filaments. For good agreement between calculated and experimental results, the deposited boron must continue to expand after deposition, and the build up of residual stresses must be limited by significant boron and carbon creep rates.
Document ID
19800011830
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Behrendt, D. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Composite Materials
Report/Patent Number
E-386
NASA-TM-81456
Report Number: E-386
Report Number: NASA-TM-81456
Meeting Information
Meeting: Ann. Conf. on Composites and Advanced Mater.
Location: Cocoa Beach, FL
Country: United States
Start Date: January 21, 1980
End Date: January 24, 1980
Sponsors: Am. Ceram. Soc.
Accession Number
80N20314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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