2011
DOI: 10.1115/1.4005191
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Predicted Response of the Die-Carrier Assembly in Flexible Electronics to the Combined Action of Tension and Bending Applied to the Carrier

Abstract: A die-carrier assembly, subjected to the external tensile forces and bending moments applied to the flexible carrier is considered. The objective of the analysis is to develop a simple, easy-to-use, and physically meaningful predictive analytical ("mathematical") model aimed at understanding the physics of the combined action of tension and bending experienced by the carrier and transmitted to the die through the more-or-less compliant ,bond. The addressed stresses include the interfacial shearing and peeling … Show more

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Cited by 9 publications
(7 citation statements)
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“…5(c)) can be obtained using the theory of lap-joints. [106][107][108] It can be noticed that Eq. (4) considers only the effect of M, and the effect of q is ignored.…”
Section: A Uniaxial Bending Of Utcsmentioning
confidence: 99%
“…5(c)) can be obtained using the theory of lap-joints. [106][107][108] It can be noticed that Eq. (4) considers only the effect of M, and the effect of q is ignored.…”
Section: A Uniaxial Bending Of Utcsmentioning
confidence: 99%
“…and has an horizontal asymptote λ ∞ k = λ e + kλ −1 e as y → +∞. Equilibrium paths predicted by (8) are traced out in the plane (y = max (w) , λ) by gradually incrementing y and evaluating λ k , k and a 0 being fixed. Predictions are compared with a numerical solution of (6), using MATLAB's boundary value solver bvp4c [this is a finite difference code that implements a collocation formula, details of which can be found in 29].…”
Section: Solving Methodsmentioning
confidence: 99%
“…The usual way to model the interaction between the beam and the foundation is to replace the latter with a set of independent springs whose restoring force is a linear [see e.g. [1][2][3][4][5][6][7][8] or a nonlinear [see e.g. 9-19] function of the local deflection of the beam.…”
Section: Introductionmentioning
confidence: 99%
“…The system is symmetric about the axes x 1 and x 2 , therefore only half of it is examined. The solution is obtained by solving the equilibrium, kinematic and constitutive equations, together with the boundary conditions, well-known in literature [11][12][13][14][15][16][17]. The applied uniform load q can be decomposed into a uniform axial stretching load (F) acting along the x 1 -axis, and a lateral load that creates a bending moment (M) about the x 2 -axis [18].…”
Section: Analytical Solutionmentioning
confidence: 99%