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Concept for Determining the Life of Ceramic Matrix Composites Using Nondestructive Characterization TechniquesDamping measurements have been taken on ceramic matrix composite (CMC) turbopump blisks in the as fabricated, post proof testing, and post turbopump testing conditions. These results indicate that damping is able to quantify fatigue of the CMC blisk. This gives hope for the potential of determining the actual and residual life of CMC materials using a combination of nondestructive techniques. If successful, then this new paradigm for life prediction of CMCs could revolutionize the approach for designing and servicing CMC components, thereby significantly reducing costs for design, development, health monitoring, and maintenance of CMC components and systems. The Nondestructive Characterization (NDC) life prediction approach would complement life prediction using micromechanics and continuum finite element models. This paper reports on the initial concept of NDC life prediction and how changes in damping and ultrasonic elastic modulus data have established the concept as a possibility.
Document ID
20000039346
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Effinger, Michael
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ellingson, Bill
(Argonne National Lab. IL United States)
Spohnholtz, Todd
(Argonne National Lab. IL United States)
Koenig, John
(Southern Research Inst. United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 2000
Subject Category
Composite Materials
Meeting Information
Meeting: 4th Aerospace Materials, Processes and Environmental Technology Conference
Location: Huntsville, AL
Country: United States
Start Date: September 18, 2000
End Date: September 21, 2000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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