Abstract. The paper presents a numerical analysis of corrugated steel plate (CSP) bridge with reinforced concrete (RC) relieving slab under static loads. Calculations were made based on the finite element method using Abaqus software. Two computation models were used; in the first one, RC slab was used, and the other was without it. The effect of RC slab to deformations of CSP shell was determined. Comparing the computational results from two numerical models, it can be concluded that when the relieving slab is applied, substantial reductions in displacements, stresses, bending moments and axial thrusts are achieved. Relative reductions of displacements were in the range of 53-66%, and stresses of 73-82%. Maximum displacements and bending moments were obtained at the shell crown, and maximum stresses and axial thrusts at the quarter points. The calculation results were also compared to the values from experimental tests. The course of computed displacements and stresses is similar to those obtained from experimental tests, although the absolute values were generally higher than the measured ones. Results of numerical analyses can be useful for bridge engineering, with particular regard to bridges and culverts made from corrugated steel plates for the range of necessity of using additional relieving elements.
The paper presents the results of numerical analysis of the behaviour under static loads of a soil-shell bridge equipped with a reinforced concrete (RC) relieving slab. The relevant calculations were carried out using Abaqus program based on finite element method (FEM). Two computational models have been derived: one with and the other without a RC relieving slab. The analysis included determination of the effect of the RC relieving slab on the steel shell made of corrugated plates. The results obtained with the two above-mentioned numerical models were compared to show that the relieving slab resulted in a considerable reduction of the displacements and stresses, namely 55-63% for displacements and 73-82% for stress). The maximum displacements occur at the shell crown while the highest stresses occur at the shell quarter-points. The results of calculations were compared with the experimental data and with the results of earlier calculations carried out with Robot Millenium program. The displacement and stress curves are close to the experimental results. Generally the absolute values of displacements and stresses were higher than the experimental data.
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