Benefits of X-Ray CMT for the Modeling of C/C Composites
C/C composites have application in very demanding areas like aerospace, fusion technology, etc. and thus their optimization is crucial, both in the control of processing routes and in the prediction of their behavior in use. Intense modeling efforts have been performed in these directions. To help a...
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Published in | Advanced engineering materials Vol. 13; no. 3; pp. 178 - 185 |
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Main Authors | , , , , |
Format | Journal Article |
Language | English |
Published |
Weinheim
WILEY-VCH Verlag
01.03.2011
WILEY‐VCH Verlag Wiley |
Series | 3D‐Imaging of Materials and Systems |
Subjects | |
Online Access | Get full text |
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Summary: | C/C composites have application in very demanding areas like aerospace, fusion technology, etc. and thus their optimization is crucial, both in the control of processing routes and in the prediction of their behavior in use. Intense modeling efforts have been performed in these directions. To help a direct application on actual materials, with possibly complex reinforcement architectures, X‐ray computerized micro‐tomography (CMT) is a beneficial technique, since it allows producing extremely detailed representations of these architectures. However, there is a long way from the crude X‐ray projections to the information that is directly usable in C/C composite modeling. This paper summarizes several achievements in this domain and discusses the obtained results, concerning (i) composites imaging by phase contrast CMT and holographic CMT, (ii) evaluation of effective geometrical and transfer properties in fiber arrangements and actual fiber‐reinforced composites, (iii) modeling of degradation by ablation, and (iv) modeling of processing by chemical vapor infiltration.
This article summarizes and discusses holotomographic and phase‐contrast X‐ray Tomographic imaging of C/C composites performed at two resolutions, and subsequent computations of geometrical and transport properties, as well as simulations, e.g., of the modeling of matrix processing by chemical vapor infiltration. |
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Bibliography: | ark:/67375/WNG-PF7JX8D5-N This work has been funded by CNRS and Snecma Propulsion Solide (Safran Group) through a grant to O. C., by the French Ministry of Education through a grant to C. M., and by CEA and CNRS through a grant to J. L. ArticleID:ADEM201000233 istex:E048B938A3F6EE8D59FFB82FAECDCD639E6CF7BE ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
ISSN: | 1438-1656 1527-2648 1527-2648 |
DOI: | 10.1002/adem.201000233 |