NASA NTRS · 20060051738
Ceramic Matrix Composite Vane Subelement Burst Testing
Abstract
Burst tests were performed on Ceramic Matrix Composite (CMC) vane specimens, manufactured by two vendors, under the Ultra Efficient Engine Technology (UEET) project. Burst specimens were machined from the ends of 76mm long vane sub-elements blanks and from High Pressure Burner Rig (HPBR) tested specimens. The results of burst tests will be used to compare virgin specimens with specimens that have had an Environmental Barrier Coating (EBC) applied, both HPBR tested and untested, as well as a comparison between vendors.
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Brewer, David N., Verrilli, Michael, Calomino, Anthony. 2006-01-01. Ceramic Matrix Composite Vane Subelement Burst Testing. https://ntrs.nasa.gov/citations/20060051738
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