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Analysis of thermomechanical fatigue of unidirectional titanium metal matrix compositesThermomechanical fatigue (TMF) data was generated for a Ti-15V-3Cr-3Al-3Sn (Ti-15-3) material reinforced with SCS-6 silicon carbide fibers for both in-phase and out-of-phase thermomechanical cycling. Significant differences in failure mechanisms and fatigue life were noted for in-phase and out-of-phase testing. The purpose of the research is to apply a micromechanical model to the analysis of the data. The analysis predicts the stresses in the fiber and the matrix during the thermal and mechanical cycling by calculating both the thermal and mechanical stresses and their rate-dependent behavior. The rate-dependent behavior of the matrix was characterized and was used to calculate the constituent stresses in the composite. The predicted 0 degree fiber stress range was used to explain the composite failure. It was found that for a given condition, temperature, loading frequency, and time at temperature, the 0 degree fiber stress range may control the fatigue life of the unidirectional composite.
Document ID
19910022363
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mirdamadi, M.
(NASA Langley Research Center Hampton, VA., United States)
Johnson, W. S.
(NASA Langley Research Center Hampton, VA., United States)
Bahei-El-din, Y. A.
(Rensselaer Polytechnic Inst. Troy, NY., United States)
Castelli, M. G.
(Sverdrup Technology, Inc., Cleveland OH., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-104105
NAS 1.15:104105
Report Number: NASA-TM-104105
Report Number: NAS 1.15:104105
Meeting Information
Meeting: ASTM Symposium on Composites Materials: Fatigue and Fracture IV
Location: Indianapolis, IN
Country: United States
Start Date: May 6, 1991
End Date: May 9, 1991
Accession Number
91N31677
Funding Number(s)
PROJECT: RTOP 505-63-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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