Physics-Based Design Tools for Lightweight Ceramic Composite Turbine Components with Durable Microstructures
- Author
- DiCarlo, James A.
- Published
- March 15, 2011.
- Physical Description
- 1 electronic document
Online Version
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- Restrictions on Access
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary
- Under the Supersonics Project of the NASA Fundamental Aeronautics Program, modeling and experimental efforts are underway to develop generic physics-based tools to better implement lightweight ceramic matrix composites into supersonic engine components and to assure sufficient durability for these components in the engine environment. These activities, which have a crosscutting aspect for other areas of the Fundamental Aero program, are focusing primarily on improving the multi-directional design strength and rupture strength of high-performance SiC/SiC composites by advanced fiber architecture design. This presentation discusses progress in tool development with particular focus on the use of 2.5D-woven architectures and state-of-the-art constituents for a generic un-cooled SiC/SiC low-pressure turbine blade.
- Other Subject(s)
- Collection
- NASA Technical Reports Server (NTRS) Collection.
- Note
- Document ID: 20110011566.
E-17753.
2011 Technical Conference; 15-17 Mar. 2011; Cleveland, OH; United States. - Terms of Use and Reproduction
- No Copyright.
View MARC record | catkey: 15990933