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    The Effect of Matrix Microstructure on Thermally Induced Residual Stresses in SiC/Titanium Aluminide Composites

    Source: Journal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 002::page 215
    Author:
    Marek-Jerzy Pindera
    ,
    Alan D. Freed
    DOI: 10.1115/1.2904276
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper examines the effect of varying the microstructural composition of titanium aluminide on the evolution of residual stresses in titanium aluminide matrix composites. An analytical model is developed to determine residual stresses in fiber and matrix phases of unidirectional, SiC/Ti-Al composites subjected to axisymmetric thermal loading. The model uses elements of the concentric cylinder model and the method of cells to calculate residual thermal stresses in the presence of temperature-dependent and inelastic behavior of the fiber and matrix phases. The concentric cylinder model is employed as a geometric model for the unidirectional composite, whereas the method of cells is employed in modeling the microstructure of the titanium aluminide matrix phase. The titanium aluminide matrix consists of distinct brittle and ductile α and β phases whose volume content is varied in the present scheme to understand how the resulting residual stresses can be altered. Both spatially uniform and nonuniform variations of the α and β phases are considered. The results explain the occurrence of radial microcracks in SiC/Ti-Al composites in the presence of a β-depleted region at the fiber/matrix interface, and validate the potential of engineering the matrix phase to reduce residual stresses in these composites.
    keyword(s): Composite materials , Residual stresses , Titanium aluminide , Fibers , Cylinders , Microcracks , Temperature , Brittleness , Thermal stresses AND Modeling ,
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      The Effect of Matrix Microstructure on Thermally Induced Residual Stresses in SiC/Titanium Aluminide Composites

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    http://yetl.yabesh.ir/yetl1/handle/yetl/113709
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    contributor authorMarek-Jerzy Pindera
    contributor authorAlan D. Freed
    date accessioned2017-05-08T23:44:26Z
    date available2017-05-08T23:44:26Z
    date copyrightApril, 1994
    date issued1994
    identifier issn0094-4289
    identifier otherJEMTA8-26963#215_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113709
    description abstractThis paper examines the effect of varying the microstructural composition of titanium aluminide on the evolution of residual stresses in titanium aluminide matrix composites. An analytical model is developed to determine residual stresses in fiber and matrix phases of unidirectional, SiC/Ti-Al composites subjected to axisymmetric thermal loading. The model uses elements of the concentric cylinder model and the method of cells to calculate residual thermal stresses in the presence of temperature-dependent and inelastic behavior of the fiber and matrix phases. The concentric cylinder model is employed as a geometric model for the unidirectional composite, whereas the method of cells is employed in modeling the microstructure of the titanium aluminide matrix phase. The titanium aluminide matrix consists of distinct brittle and ductile α and β phases whose volume content is varied in the present scheme to understand how the resulting residual stresses can be altered. Both spatially uniform and nonuniform variations of the α and β phases are considered. The results explain the occurrence of radial microcracks in SiC/Ti-Al composites in the presence of a β-depleted region at the fiber/matrix interface, and validate the potential of engineering the matrix phase to reduce residual stresses in these composites.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of Matrix Microstructure on Thermally Induced Residual Stresses in SiC/Titanium Aluminide Composites
    typeJournal Paper
    journal volume116
    journal issue2
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2904276
    journal fristpage215
    journal lastpage221
    identifier eissn1528-8889
    keywordsComposite materials
    keywordsResidual stresses
    keywordsTitanium aluminide
    keywordsFibers
    keywordsCylinders
    keywordsMicrocracks
    keywordsTemperature
    keywordsBrittleness
    keywordsThermal stresses AND Modeling
    treeJournal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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