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Proc. ASME. PVP2005, Volume 4: Fluid Structure Interaction, 807-817, July 17–21, 2005
Paper No: PVP2005-71700
... in relation to shock data derived from existing flyer plate impact test data. An orthotropic Equation of State  has also been implemented into the LS-DYNA3D code. A flyer plate test is simulated using the implemented model, and with material parameters derived using the theory of mixture approach...