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CMC Research at NASA Glenn in 2019: Recent Progress and PlansAs part of NASA's Aeronautics research, Glenn Research Center has developed SiC/SiC Ceramic Matrix Composites (CMC) for 2700 degrees Fahrenheit turbine engine applications in the next generation of ultra-efficient aircraft. In this presentation, the development of fiber and matrix constituents and fabrication processes that enabled this advancement will be reviewed, and characterization of the resulting improvements in CMC mechanical properties and durability will be summarized. Progress toward the development and validation of models predicting the effects of the engine environment on durability of Ceramic Matrix Composites and Environmental Barrier Coatings will be summarized. Results from current collaborative research with industry and other government agencies will be reviewed. Research plans for 2019 and opportunities for future collaborations with NASA will also be summarized.
Document ID
20190001446
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Grady, Joseph E.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
March 12, 2019
Publication Date
January 28, 2019
Subject Category
Composite Materials
Report/Patent Number
GRC-E-DAA-TN64864
Meeting Information
Meeting: Annual Conference on Composites, Materials and Structures
Location: Cocoa Beach, FL
Country: United States
Start Date: January 28, 2019
End Date: January 31, 2019
Sponsors: United States Advanced Ceramics Association
Funding Number(s)
WBS: WBS 081876.02.03.50.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Composites
Propulsion Materials
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