2018
DOI: 10.1016/j.compositesb.2018.04.035
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Bending models for superelastic shape memory alloy laminated composite cantilever beams with elastic core layer

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Cited by 20 publications
(22 citation statements)
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“…The equations of the shape functions are obtained by using the following assumed forms of the slope and displacements [29] :…”
Section: Tmmentioning
confidence: 99%
“…The equations of the shape functions are obtained by using the following assumed forms of the slope and displacements [29] :…”
Section: Tmmentioning
confidence: 99%
“…The formulation of the volume fraction z as function of the coordinate y , measured with respect to the neutral axis within the transformed region, is assumed to obey the following linear relation (Viet et al, 2018b)…”
Section: Modeling the Sma/fgm Cantilever Beammentioning
confidence: 99%
“…The stress thresholds for the beginning and the end of reverse transformation at a point where a volume fraction z = z * ei ± was achieved during loading are calculated by letting z equal z * ei ± and 0, respectively (Viet et al, 2018b), in equation (1). Then the following relations are obtained…”
Section: Modeling the Sma/fgm Cantilever Beammentioning
confidence: 99%
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