NASA NTRS · 19920032942
Impact design methods for ceramic components in gas turbine engines
Abstract
Methods currently under development to design ceramic turbine components with improved impact resistance are presented. Two different modes of impact damage are identified and characterized, i.e., structural damage and local damage. The entire computation is incorporated into the EPIC computer code. Model capability is demonstrated by simulating instrumented plate impact and particle impact tests.
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Song, J., Cuccio, J., Kington, H.. 1991-06-01. Impact design methods for ceramic components in gas turbine engines. https://ntrs.nasa.gov/citations/19920032942
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