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Hoop Tensile Properties of Ceramic Matrix Composite CylindersTensile stress-strain properties in the hoop direction were obtained for 100-mm diameter SiC/SiC ceramic matrix composite cylinders using ring specimens machined form the cylinder ends. The cylinders were fabricated from 2D balanced SiC fabric with several material variants, including wall thickness (6,8, and 12 plies), SiC fiber type (Sylramic, Sylramic-iBN, Hi-Nicalon, and Hi-Nicalon S), fiber sizing type, and matrix type (full CVI SiC, and partial CVI SiC plus slurry cast + melt-infiltrated SiC-Si). Fiber ply splices existed in all the hoops. Tensile hoop measurements are made at room temperature and 1200 C using hydrostatic ring test facilities. The failure mode of the hoops, determined through microstructural examination, is presented. The hoop properties are compared with in-plane data measured on flat panels using same material variants, but containing no splices.
Document ID
20050051727
Acquisition Source
Headquarters
Document Type
Preprint (Draft being sent to journal)
Authors
Verrilli, Michael J.
(NASA Glenn Research Center Cleveland, OH, United States)
DiCarlo, James A.
(NASA Glenn Research Center Cleveland, OH, United States)
Yun, HeeMan
(NASA Glenn Research Center Cleveland, OH, United States)
Barnett, Terry
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Report/Patent Number
Paper-1234
Report Number: Paper-1234
Funding Number(s)
OTHER: 714-30-18
Distribution Limits
Public
Copyright
Public Use Permitted.
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