Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
783684 | International Journal of Impact Engineering | 2007 | 23 Pages |
Abstract
This two part paper examines the behaviour of fibre-metal laminates (FMLs) subjected to localised explosive blast loading. Part I presents the experimental observations of diamond and cross-shaped back face deformation, as well as pitting, global displacement and ring-buckling of the front face are also discerned. Part II presents quantitative analysis of the experimental data. When expressed in terms of non-dimensional parameters front and back face displacements fall within one plate thickness of a linear trend line. The threshold impulse for the onset of tearing is found to increase linearly with panel thickness.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Mechanical Engineering
Authors
S.L. Lemanski, G.N. Nurick, G.S. Langdon, M.C. Simmons, W.J. Cantwell, G.K. Schleyer,