Practical techniques for finite element modeling to simulate structural crashworthiness in ship collisions and grounding (Part I: Theory)
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...This is based on a literature search where it is indicated that the aluminium is essentially strain rate insensitivity [24,25], and that the effect of viscoplasticity is very small for high tensile steels since material constant C of the Cowper-Symonds constitutive equation is quite large (3200 s ) [26]....
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...The true strain and stress relation until failure is traced by Hoffmann and Vogl [16], Huatao and Roehr [2], Joun et al. [17], Koc and Stok [18], Ling [19], Mirone [20], and Paik [21], but no prediction of the failure strain and finite element length dependency is presented....
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...[17], Koc and Stok [18], Ling [19], Mirone [20], and Paik [21], but no prediction of the failure strain and finite element length dependency is presented....
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References
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...As shown in the figure, however, material model II overestimates the strain-hardening characteristics, although the necking behavior is more properly accounted for than for model I. 71C© Woodhead Publishing Ltd doi:10.1533/saos.2006.148 SAOS 2007 Vol. 2 No. 1 Material model III In this paper, a brand new approach called the knockdown factor approach is proposed....
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...When the mesh size is infinitely small, the critical fracture strain 73C© Woodhead Publishing Ltd doi:10.1533/saos.2006.148 SAOS 2007 Vol. 2 No. 1 εfc to be defined for FE structural modeling may be several times larger than the nominal fracture strain εf obtained from the material tensile coupon test results, and it approaches the same value of εf as the FE mesh size increases....
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...The curve of ‘simulation’ in Figure 6 is reverted from the true stress–train curve expressed by 72SAOS 2007 Vol. 2 No. 1 doi:10.1533/saos.2006.148 C© Woodhead Publishing Ltd Equation (4) together with Equation (5), and shows a very good agreement with the curve of ‘experiment,’ which was directly obtained from the tensile coupon test, confirming that material model III is valid....
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...A number of analytical formulae are available to predict the expected length of one structural fold, e.g., Amdahl and Kavlie (1992), Wierzbicki and Abramowicz (1983), Wierzbicki et al. (1993), Paik and Pedersen (1995), Wang and Ohtsubo (1997), and Suzuki et al. (2000), among others, and Paik and…...
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...The friction coefficient in the simulation of grounding or 76SAOS 2007 Vol. 2 No. 1 doi:10.1533/saos.2006.148 C© Woodhead Publishing Ltd collisions is often determined by an empirical approach, depending on the accident situation....
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"Practical techniques for finite ele..." refers background in this paper
...Inertia effects Inertia effects may sometimes be needed for impact response simulations of thin-walled structures (Reid and Reddy 1983; Harrigan et al. 1999; Paik and Chung 1999; Karagiozova et al. 2000)....
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...Inertia effects may sometimes be needed for impact response simulations of thin-walled structures (Reid and Reddy 1983; Harrigan et al. 1999; Paik and Chung 1999; Karagiozova et al. 2000)....
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