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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 (CVD) 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 to show how the principal residual stresses and the filament elongation vary as the parameters defining deposition strain and creep are varied. The calculated results are compared with experimental axial residual stress and elongation measurements made on B/C filaments. This comparison requires that for good agreement between calculated and experimental results, the deposited boron must continue to expand after deposition, and that the build-up of residual stresses is limited by significant boron and carbon creep rates.
Document ID
19800060067
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Behrendt, D. R.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Composite Materials
Meeting Information
Meeting: Annual Conference on Composites and Advanced Materials
Location: Cocoa Beach, FL
Start Date: January 21, 1980
End Date: January 24, 1980
Sponsors: American Ceramic Society
Accession Number
80A44237
Distribution Limits
Public
Copyright
Other

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