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Thermal stress effects in intermetallic matrix compositesIntermetallic matrix composites develop residual stresses from the large thermal expansion mismatch (delta-alpha) between the fibers and matrix. This work was undertaken to: establish improved techniques to measure these thermal stresses in IMC's; determine residual stresses in a variety of IMC systems by experiments and modeling; and, determine the effect of residual stresses on selected mechanical properties of an IMC. X ray diffraction (XRD), neutron diffraction (ND), synchrotron XRD (SXRD), and ultrasonics (US) techniques for measuring thermal stresses in IMC were examined and ND was selected as the most promising technique. ND was demonstrated on a variety of IMC systems encompassing Ti- and Ni-base matrices, SiC, W, and Al2O3 fibers, and different fiber fractions (Vf). Experimental results on these systems agreed with predictions of a concentric cylinder model. In SiC/Ti-base systems, little yielding was found and stresses were controlled primarily by delta-alpha and Vf. In Ni-base matrix systems, yield strength of the matrix and Vf controlled stress levels. The longitudinal residual stresses in SCS-6/Ti-24Al-llNb composite were modified by thermomechanical processing. Increasing residual stress decreased ultimate tensile strength in agreement with model predictions. Fiber pushout strength showed an unexpected inverse correlation with residual stress. In-plane shear yield strength showed no dependence on residual stress. Higher levels of residual tension led to higher fatigue crack growth rates, as suggested by matrix mean stress effects.
Document ID
19940012045
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wright, P. K.
(General Electric Co. Cincinnati, OH, United States)
Sensmeier, M. D.
(General Electric Co. Cincinnati, OH, United States)
Kupperman, D. S.
(Argonne National Lab. IL., United States)
Wadley, H. N. G.
(Virginia Univ. Charlottesville., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1993
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NAS 1.26:191191
NASA-CR-191191
E-8127
Report Number: NAS 1.26:191191
Report Number: NASA-CR-191191
Report Number: E-8127
Accession Number
94N16518
Funding Number(s)
PROJECT: RTOP 510-01-50
CONTRACT_GRANT: NAS3-25790
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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