1986
DOI: 10.1007/bf01523075
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Calculation of stresses in shells under local loads by the method of S. P. Timoshenko

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Cited by 7 publications
(6 citation statements)
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“…In this case, the strain, calculated from the theory of pure bending of a plate to a cylindrical surface valid between the inner loading points, is equal to ε = 3dz 5a 2 , where d is thickness, z is the displacement of the inner loading bars and a is the distance between the first and second points of the four-point bending load cell (a = 10 mm) [12]. The GF T was calculated for the four upward cycles of the z displacement versus time and resistance curves experimentally acquired for each one of the samples.…”
Section: Electromechanical Characterization Of Composites 241 Testing...mentioning
confidence: 99%
“…In this case, the strain, calculated from the theory of pure bending of a plate to a cylindrical surface valid between the inner loading points, is equal to ε = 3dz 5a 2 , where d is thickness, z is the displacement of the inner loading bars and a is the distance between the first and second points of the four-point bending load cell (a = 10 mm) [12]. The GF T was calculated for the four upward cycles of the z displacement versus time and resistance curves experimentally acquired for each one of the samples.…”
Section: Electromechanical Characterization Of Composites 241 Testing...mentioning
confidence: 99%
“…where M and κ = dϕ/ds are the bending moment and the curvature at any point of the beam, respectively, and I is the moment of inertia of the beam cross section about the neutral axis [2][3][4]. We will consider the deflections of a cantilever beam subjected to one vertical concentrated load at the free end by supposing that the deflection due to its self-weight is zero.…”
Section: Theoretical Analysismentioning
confidence: 99%
“…The mathematical treatment of the equilibrium of cantilever beams does not involve a great degree of difficulty [2][3][4]. Nevertheless, unless small deflections are considered, an analytical solution does not exist, since for large deflections a differential equation with a non-linear term must be solved.…”
Section: Introductionmentioning
confidence: 99%
“…Recent work by (Paglietti and Carta, 2009) has concerns over the use of such method. The theoretical basis for stress distributions in tapered beams in elastic range is investigated (Timoshenko, 1930; Oden, 1967).…”
Section: Shear Strength Verificationmentioning
confidence: 99%