1968
DOI: 10.2534/jjasnaoe1968.1968.124_183
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Elastic-Plastic Analysis of Framed Structures using the Matrix Method

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Cited by 12 publications
(7 citation statements)
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“…Using the first order approximation of the residual via (35) and (36) and setting it equal to zero in combination with the consistency condition (37) gives the equation system …”
Section: Robust Return Algorithm Including Distributed Loadsmentioning
confidence: 99%
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“…Using the first order approximation of the residual via (35) and (36) and setting it equal to zero in combination with the consistency condition (37) gives the equation system …”
Section: Robust Return Algorithm Including Distributed Loadsmentioning
confidence: 99%
“…In the first iteration an estimate of ∆λ is calculated as well via (11) whereu t is replaced by ∆ũ t . Subsequently the residual is calculated via (35) and if the residual is sufficiently small and none of the yield conditions are violated, the predicted state is accepted. If the residual is not sufficiently small a midpoint state is determined by making half a step using (40) and (41) with rũ/2 and f y /2.…”
Section: Determine (∂mentioning
confidence: 99%
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“…earthquake response analysis, taking into account some kind of degradation effect (Inglessis et al 1999;Kaewkulchai and Williamson 2004). The theory of plastic hinges was introduced in the late 1960's for both monotonic loading (Ueda et al 1968), and cyclic loading with large displacements (Ueda et al 1969). The elastic tangent stiffness matrix in a large displacement but small deformation theory was derived in (Oran 1973) with the use of an equilibrium format of the beam.…”
Section: Introductionmentioning
confidence: 99%
“…Hence some kind of correction has to be applied on the magnitude of load increments. When Mises yield criterion is applied to plane stress problems, such a load magnification factor can be determined from the following equation : ( 4 ) where a: load magnification factor ay, rxy: stress components at the (n 1)th step Jax, Jay, 4rxy : increments of stress components at the nth step : yield stress of the material From Eq. ( 4 ), a is evaluated in the following form : It is known that the load magnification factor, a, is a function of the stress, (a), at the (n-1)th step, the stress increment, {Jo.…”
Section: Introductionmentioning
confidence: 99%