Evaluation of the SPH method for the modelling of spall in anisotropic alloys

dc.contributor.authorDe Vuyst, Tom-
dc.contributor.authorVignjevic, Rade-
dc.contributor.authorBourne, Neil K.-
dc.contributor.authorCampbell, James C.-
dc.date.accessioned2011-11-13T23:22:55Z
dc.date.available2011-11-13T23:22:55Z
dc.date.issued2005-06-27T00:00:00Z-
dc.description.abstractSpall caused by hypervelocity impacts at the lower range of velocities could result in significant damage to spacecraft. A number of polycrystalline alloys, used in spacecraft manufacturing, exhibit a pronounced anisotropy in their mechanical properties. The aluminium alloy AA 7010, whose orthotropy is a consequence of the meso-scale phase distribution or grain morphology, has been chosen for this investigation. The material failure observed in plate impact was simulated using an explicit finite element code and a smoothed particle hydrodynamics (SPH) code. A number of spall models where used, and the Hugoniot Elastic Limit (HEL) and spall strength have been studied as a function of orientation, and compared to experimental results.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/879
dc.titleEvaluation of the SPH method for the modelling of spall in anisotropic alloysen_UK
dc.typeConference paper-

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