2013
DOI: 10.1177/1464420713499484
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Experimental failure investigation for a titanium metal matrix composite with +45° and ±45° fibre orientations

Abstract: This paper presents the results of micromechanical failure analyses of titanium metal matrix composite shafts, under cyclic torsional loading. Two different fibre orientations were used to investigate the failure mechanisms, namely þ45 and AE45 fibre orientations. The fracture surfaces, after fatigue testing, were examined using a scanning electron microscope. Evidence was found of the existence of both ductile failure which occurred in the matrix material and brittle failure which occurred in the fibres. Thes… Show more

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Cited by 4 publications
(16 citation statements)
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“…Figure 13 shows the stress distribution obtained for the case of frictionless contact. The fibre volume fraction is 35% and the tensile loading is 859 MPa, as described in Hyde et al 3 This is similar to the loading experienced in the TiMMC layer of a shaft which was tested under fatigue loading conditions, described in Hyde et al 15…”
Section: Fe Results and Discussion For The +45° Fibre Orientationsupporting
confidence: 56%
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“…Figure 13 shows the stress distribution obtained for the case of frictionless contact. The fibre volume fraction is 35% and the tensile loading is 859 MPa, as described in Hyde et al 3 This is similar to the loading experienced in the TiMMC layer of a shaft which was tested under fatigue loading conditions, described in Hyde et al 15…”
Section: Fe Results and Discussion For The +45° Fibre Orientationsupporting
confidence: 56%
“…In addition, surface-to-surface contact conditions are prescribed at the fibre-matrix interface. The loads are chosen to approximately represent the torsional shaft loading, as explained in Hyde et al 3 Unit cell analysis for the 645°fibre orientation Unit cell geometry. With regard to the 645°fibre directions, illustrated in Figure 7, a unit cell can be devised, as shown in Figure 8.…”
Section: Methodsmentioning
confidence: 99%
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“…It is generally known that materials may experience failure at a stress level lower than their static strength when subjected to dynamic loadings. [1][2][3][4][5][6][7][8][9][10] In other words, applied loads cyclic in nature may reduce the strength of materials such as metals, plastics, and composites. Estimation and prediction of the degree of damage after loading is one of the most important design characteristics as this knowledge results in a prudent, optimum, and safe structure.…”
Section: Introductionmentioning
confidence: 99%