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tesi A. Caggiano.pdf - EleA@UniSA - Università degli Studi di Salerno

tesi A. Caggiano.pdf - EleA@UniSA - Università degli Studi di Salerno

tesi A. Caggiano.pdf - EleA@UniSA - Università degli Studi di Salerno

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List of Figures7.9 Load-C T ODm numerical pre<strong>di</strong>ctions against the experimental data on SFRCS100-type by <strong>Caggiano</strong> et al. [2012a]. . . . . . . . . . . . . . . . . . . . . . . . 1508.1 (a) Concrete specimen, (b) continuum <strong>di</strong>scretization scale, (c) 4-node continuumFE and (d) spherical microplane region at gauss-point with a generalizednormal <strong>di</strong>rection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1558.2 Strain and stress components at the microplane level. . . . . . . . . . . . . . . 1568.3 Maximum strength criteria and plastic flow rules. . . . . . . . . . . . . . . . . 1608.4 S[ξ # ] scaling function of the microplane model in terms of the ξ # parameter,where the # symbol = χ mi c ,c mi c , tan(α mi c ) or σ N ,C AP . . . . . . . . . . . . . . 1628.5 ξ # functions, with # = χ mi c ,c mi c , tan(α mi c ) or σ N ,C AP , depen<strong>di</strong>ng on the workspent-to-fracture energy ratio, w cr /G I f or w cr /G I I a . . . . . . . . . . . . . . . . 163f8.6 Yiel<strong>di</strong>ng criteria at <strong>di</strong>fferent ratios between work spent values and fracture energies:(w crG I f, w crG I I af)= (0.0,0.0), (0.2,0.1), (0.4,0.2), (0.6,0.3), (0.8,0.4), (1.0,0.5),(1.0,0.6), (1.0,0.8) (from the biggest size up to smallest one). . . . . . . . . . . 1638.7 Microplane strain activating the fiber bridging effects. . . . . . . . . . . . . . . 1658.8 Load configurations and restraint con<strong>di</strong>tions for uniaxial tension and simpleshear. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1668.9 Comparison between the numerical pre<strong>di</strong>ctions and the experimental results(dotted curves) by Li and Li [2001] of SFRCs with “Dramix type I” and “type II”. 1678.10 Interface-based simulations vs. microplane ones under tensile load cases. . . . 1698.11 Lateral shear load - <strong>di</strong>splacement by considering several integration points(varying from 2 to 25) and fiber percentages. . . . . . . . . . . . . . . . . . . . 1708.12 Lateral shear load - <strong>di</strong>splacement comparisons when several microplane numbersand fiber contents are considered. . . . . . . . . . . . . . . . . . . . . . . 171xix

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