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Micromechanics of composites with shape memory alloy fibers in uniform thermal fieldsAnalytical procedures are developed for a composite system consisting of shape memory alloy fibers within an elastic matrix subject to uniform temperature fluctuations. Micromechanics for the calculation of the equivalent properties of the composite are presented by extending the multi-cell model to incorporate shape memory alloy fibers. A three phase concentric cylinder model is developed for the analysis of local stresses which includes the fiber, the matrix, and the surrounding homogenized composite. The solution addresses the complexities induced by the nonlinear dependence of the in-situ martensite fraction of the fibers to the local stresses and temperature, and the local stresses developed from interactions between the fibers and matrix during the martensitic and reverse phase transformations. Results are presented for a nitinol/epoxy composite. The applications illustrate the response of the composite in isothermal longitudinal loading and unloading, and in temperature induced actuation. The local stresses developed in the composite under various stages of the martensitic and reverse phase transformation are also shown.
Document ID
19950026789
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Birman, Victor
(Missouri Univ. Rolla, MO., United States)
Saravanos, Dimitris A.
(Ohio Aerospace Inst. Cleveland, OH., United States)
Hopkins, Dale A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:107011
E-9795
NASA-TM-107011
AIAA PAPER 95-1210
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: New Orleans, LA
Country: United States
Start Date: April 10, 1995
End Date: April 13, 1995
Accession Number
95N33210
Funding Number(s)
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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