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Civil-Comp Proceedings
ISSN 1759-3433 CCP: 79
PROCEEDINGS OF THE SEVENTH INTERNATIONAL CONFERENCE ON COMPUTATIONAL STRUCTURES TECHNOLOGY Edited by: B.H.V. Topping and C.A. Mota Soares
Paper 44
Numerical Models Concerning Structures with Multi-Layered Textile Strengthening B. Möller, W. Graf, A. Hoffmann and F. Steinigen
Department of Civil Engineering, Institute of Statics and Dynamics of Structures, Technische Universität Dresden, Germany , "Numerical Models Concerning Structures with Multi-Layered Textile Strengthening", in B.H.V. Topping, C.A. Mota Soares, (Editors), "Proceedings of the Seventh International Conference on Computational Structures Technology", Civil-Comp Press, Stirlingshire, UK, Paper 44, 2004. doi:10.4203/ccp.79.44
Keywords: nonlinear FE-analysis, textile strengthening, ultimate limit load.
Summary
Composite constructions with textile reinforcement provide a possible means of
increasing the load-bearing capacity of existing structures. New textile technologies
permit the effective production of textile surface structures with several layers of
filament threads made of glass or carbon.
Although this new type of reinforcement applied to the surface of existing structures has proved to be highly effective, clarification is still required concerning the modified load-bearing behaviour and an assessment of structural safety. Besides experimental verifications, numerical parameter studies are especially suitable for this purpose. These permit the systematic variation of a wide range of parameters at low cost. This paper is mainly devoted to improved computational algorithms to account for the load-bearing reserves of reinforced concrete structures with textile reinforcement. For non-linear FE simulation the load bearing behaviour of the composite construction the layered model with a single reference plane (hybrid finite elements with assumed stress distribution), which has been in use for many years, is extended in such a way that several discrete, coupled, parallel reference planes may be introduced (multi reference plane model). The ensuring non rigid coupling (including delamination) between the reference planes is achieved using kinematic and static coupling conditions (interface), which are realized with the aid of bar or folded plate elements. The transfer of tensile stresses is possible up to the point of attainment of the composite stress. In the incremental iterative solution procedure a modified Newton-Raphson method was applied up to the ultimate load or alternatively, an arc length method after Ramm (also applicable to the post ultimate load behaviour). The subsequent strengthening of a construction represents a change in the static system during a loading process. The numerical simulation of the load-bearing behaviour after the stengthening is carried out with a changed static system considering the displacements, strains, stresses and material damages that appeared until then. The multi-reference plane model was verified at experiments (plates, u-profile) and applied to real construction (slab-and-beam floor, arched shell). References
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