Damage Assessment Due to Single Slamming of Foam Core Sandwich Composites

Abstract

Foam core sandwich composite panels were slammed onto the body of calm water as a function of slamming energy (161—779 J) and deadrise angle (0°—45°). Higher slamming energy and lower deadrise angle resulted in greater damage to the material. Discrete pressure data though critical in ship design, failed to yield any relevant damage information. Catastrophic failure was observed to occur beyond a threshold strain of 0.0035 mm/mm. With the introduction of a hydroelasticity function, quasi-static analysis accurately predicted strain behavior under slamming. Post-failure analysis of noncatastrophically damaged specimens indicated very little reduction in flexural capacity in spite of a measurable change in the acoustic emission activity. Core shear along the interface with the facesheets and local buckling of the facesheet and resin fragmentation were observed to be the dominant modes of failure under slamming.