Abstract:rather t.han the general elise, so that. ill the chapter on inst.ability of two-phase fl ow 1i0 reference is made, for example, to the (a ward-winning) 1963 paper of Ost.mch and Koestel.For a long t.ime it has been 11 fact that our unders(.a nding of the physics involved in vapor formation a nd tra nsport is insufficien t even \.0 p el'mit satisfactory determination of empirical relation-~hips ba.•ed, say, on dim ensional analysis. The recent advances in the cloud physics of bubbles in boi ling have not been s… Show more
“…The last example is that of a simple two‐span beam subjected to repeated cyclic load applications. Instead of the traditional textbook line model with plastic hinges (e.g., ), we represented the structure as a 2D model with plane stress mixed elements satisfying a von Mises material.…”
Section: Numerical Examplesmentioning
confidence: 99%
“…The final example demonstrates the capability of our proposed direct complementarity scheme to cater for nonmonotonic load histories that can lead to substantial changes in stress directions. A classical text book example of a two‐span beam (Figure (a)) under repeated cyclic loads (see, e.g., ) was considered for this purpose. However, instead of the traditional line element with lumped plasticity (hinges), we modeled the beam as a 2D structure with plane stress mixed elements, obeying the von Mises perfectly plastic condition.…”
“…The last example is that of a simple two‐span beam subjected to repeated cyclic load applications. Instead of the traditional textbook line model with plastic hinges (e.g., ), we represented the structure as a 2D model with plane stress mixed elements satisfying a von Mises material.…”
Section: Numerical Examplesmentioning
confidence: 99%
“…The final example demonstrates the capability of our proposed direct complementarity scheme to cater for nonmonotonic load histories that can lead to substantial changes in stress directions. A classical text book example of a two‐span beam (Figure (a)) under repeated cyclic loads (see, e.g., ) was considered for this purpose. However, instead of the traditional line element with lumped plasticity (hinges), we modeled the beam as a 2D structure with plane stress mixed elements, obeying the von Mises perfectly plastic condition.…”
“…The application of limit analysis and plasticity to structural safety concerns a wide range of engineering fields. Starting from the pioneer works of Prager, Drucker, and Greenberg's [1,2] and Massonnet and Save [3,4] that address the plastic response of structures introducing the collapse calculation for one-dimensional beams assembly as the main topic the matter has been formalized in the mathematical treatise of Hill [5], a two-fold approach is the way the limit analysis has been applied. The first, the kinematic method, consists of finding the collapse load as the load infimum among that in equilibrium with the stress linked to a compatible collapse mechanism.…”
Abstract. This work deals with the limit analysis of structures through the lower-bound theorem, using dislocations based finite elements and eigenstress modelling. The lower bound approach is based on the knowledge of the self-equilibrated stresses that constitutes the basis of the domain where the optimal solution should be searched. A twofold strategy can be used to get self-equilibrated stresses, i.e., eigenstresses. The first one pursues the calculation of the self-equilibrated stress through the numerical approximation of the differential equilibrium equation in homogeneous form through an a posteriori discretization that used polynomial representation of finite degree. The second one consists of Finite Element implementation of the self-equilibrated stress calculation by discontinuous finite elements based on Volterra's dislocations theory. Both the formulations are written in terms of the strain and precisely in terms of the strain nodal displacement parameters. Consequently, it is possible to formulate an iterative procedure starting from the knowledge of the dislocation at the incoming collapse, in Melan’s residual sense, and calculate the structural ductility requirement. Several numerical examples are presented to confirm the method's feasibility.
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