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Mechanical Characterization and Micromechanical Modeling of Woven Carbon/Copper CompositesThe present investigation examines the in-plane mechanical behavior of a particular woven metal matrix composite (MMC); 8-harness (8H) satin carbon/copper (C/Cu). This is accomplished via mechanical testing as well as micromechanical modeling. While the literature is replete with experimental and modeling efforts for woven and braided polymer matrix composites, little work has been done on woven and braided MMC's. Thus, the development and understanding of woven MMC's is at an early stage. 8H satin C/Cu owes its existence to the high thermal conductivity of copper and low density and thermal expansion of carbon fibers. It is a candidate material for high heat flux applications, such as space power radiator panels. The experimental portion of this investigation consists of monotonic and cyclic tension, compression, and Iosipescu shear tests, as well as combined tension-compression tests. Tests were performed on composite specimens with three copper matrix alloy types: pure Cu, Cu-0.5 weight percent Ti (Cu-Ti), and Cu-0.7 weight percent Cr (Cu-Cr). The small alloying additions are present to promote fiber/matrix interfacial bonding. The analytical modeling effort utilizes an approach in which a local micromechanical model is embedded in a global micromechanical model. This approach differs from previously developed analytical models for woven composites in that a true repeating unit cell is analyzed. However, unlike finite element modeling of woven composites, the geometry is sufficiently idealized to allow efficient geometric discretization and efficient execution.
Document ID
19970024964
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bednarcyk, Brett A.
(Virginia Univ. Charlottesville, VA United States)
Pindera, Marek-Jerzy
(Virginia Univ. Charlottesville, VA United States)
Ellis, David L.
(NASA Lewis Research Center Cleveland, OH United States)
Miner, Robert V.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 17, 2013
Publication Date
April 1, 1997
Publication Information
Publication: Physics and Process Modeling (PPM) and Other Propulsion R and T
Volume: 1
Subject Category
Composite Materials
Report/Patent Number
Paper-9-Vol-1
Accession Number
97N24663
Funding Number(s)
CONTRACT_GRANT: NAG3-1319
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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