Effect of coupon geometry and preload on flexural properties of oxide ceramic matrix composites
Author:
Affiliation:
1. Institute of Structures and Design German Aerospace Center Stuttgart Stuttgart Germany
2. Schunk Kohlenstofftechnik GmbH Heuchelheim Germany
3. Institute of Material Research German Aerospace Center Cologne Germany
Publisher
Wiley
Subject
Materials Chemistry,Marketing,Condensed Matter Physics,Ceramics and Composites
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1111/ijac.14307
Reference28 articles.
1. LewisD.Future opportunities and critical needs for advanced ceramics and ceramic matrix composites in aerospace applications. In:JessenT UstundagE editors.24th annual conference on composites advanced ceramics materials and structures: a ceramic engineering and science proceedings Vol.21(3).Hoboken NJ USA;2000. p.2–14.
2. VolkmannE.Effects of high‐temperature exposure on the mechanical performance of polymer‐derived oxide‐based ceramic matrix composites.Berlin:Elsevier;2015.
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