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Hoop tensile properties of ceramic matrix composite cylinders
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Verrilli, Michael J. Yun, HeeMan DiCarlo, James A. Barnett, Terry |
| Copyright Year | 2004 |
| Description | Tensile 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. |
| File Size | 4987765 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050051727 |
| Archival Resource Key | ark:/13960/t39073600 |
| Language | English |
| Publisher Date | 2004-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Hoops Panels Ceramic Matrix Composites Failure Modes Silicon Carbides Mechanical Properties Circular Cylinders Fabrication Hydrostatics Stress-strain Relationships Ply Orientation Microstructure Cross Sections Tensile Properties Slurries Room Temperature Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
