Title of article :
Higher-order dynamic response of composite sandwich panels with flexible core under simultaneous low-velocity impacts of multiple small masses
Author/Authors :
K. Malekzadeh، نويسنده , , M.R. Khalili، نويسنده , , R. Olsson، نويسنده , , A. Jafari، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2006
Abstract :
Small mass impactors, such as runway debris and hailstones may result in a wave controlled local response, which is
essentially independent of boundary conditions. The higher-order impact model of sandwich beams presented by Mijia
and Pizhong [Mijia, Y., Pizhong, Q., 2005. Higher-order impact modeling of sandwich structures with flexible core. International
Journal of Solids and Structures 42 (10), 5460–5490] is developed and enhanced to impact analysis of sandwich
panels with transversely flexible cores. Therefore, an improved fully dynamic higher-order impact theory is developed to
analyze the low-velocity impact dynamic of a system which consists of a composite sandwich panel with transversely flexible
core and multiple small impactors with small masses. Impacts are assumed to occur normally and simultaneously over
the top face-sheet with arbitrary different masses and initial velocities of impactors. The contact forces between the panel
and the impactors are treated as the internal forces of the system. First shear deformation theory (FSDT) is used for the
face-sheets while three-dimensional elasticity is used for the soft core. The fully dynamic effects of the core layer and the
face-sheets are considered in this study. Contact area can be varied with contact duration. The results in multiple mass
impacts over sandwich panels that are hitherto not reported in the literature are presented based on proposed improved
higher-order sandwich plate theory (IHSAPT). Finally, for the case study of the single mass impact, the numerical results
of the analysis have been compared either with the available experimental results or with some theoretical results. As no
literature could be found on the impact of multiple impactors over sandwich panels, the present formulation is validated
indirectly by comparing the response of two cases of double small masses and single small mass impacts. Also, in order to
demonstrate the applicability of the validation, the analytical relation of minimum distance between two impactors is
derived based on Olsson’s wave control principle in this paper.
Keywords :
Multiple masses , Core flexibility , Low-velocity impact , Higher-order model , sandwich panel
Journal title :
International Journal of Solids and Structures
Journal title :
International Journal of Solids and Structures