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Article type: Research Article
Authors: Lloyd Hammond, | Raphael Grzebieta,
Affiliations: Aeronautical and Maritime Research Laboratory, Defence Science and Technology Organisation, Melbourne, Victoria, Australia | Department of Civil Engineering, Monash University, Clayton, Victoria, Australia
Note: [] Aeronautical and Maritime Research Laboratory, Defence Science and Technology Organisation, GPO Box 4331, Melbourne, Victoria 3001, Australia. Tel.: +61 3 9626 8754; Fax: +61 3 9626 8999; E-mail: [email protected]
Abstract: The LS-DYNA/USA (Underwater Shock Analysis) coupled finite element codes are being investigated as a tool for predicting the local response of compliant plate structures subjected to far-field underwater explosion. It had previously been observed in LS-DYNA/USA models that extraneous pressure build-ups emanating from the DAA (doubly asymptotic approximation) boundaries may occur in the surrounding fluid region of the model, which inevitably lead to erroneous modelling of fluid-structure interaction and inaccurate structural responses. These instabilities typically result in divergence of the solution and eventually premature termination of the simulation. After a comprehensive investigation, it was found that the instabilities did not arise if the finite element model was hydrostatically initialised before conducting the LS-DYNA/USA simulation. The purpose of this study is to investigate the need for achieving hydrostatic equilibrium prior to the modelling of the shock wave propagation through the fluid-structure media. The method for achieving static equilibrium with the current version of the LS-DYNA/USA software is presented. The example simulations presented show that the hydrostatic initialisation procedure is effective in removing instabilities occurring at the DAA-fluid boundary, associated with the USA ambient hydrostatic pressure condition.
Keywords: underwater shock, hydrostatic initialisation, LS-DYNA/USA, DAA, finite element, structural response, dynamic loading, instabilities
Journal: Shock and Vibration, vol. 7, no. 2, pp. 57-65, 2000
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