Behaviour of fibre metal laminates subjected to localised blast loading-Part II: Quantitative analysis

Tipo de material: Texto

TextoSeries ; International Journal of Impact Engineering, 34(7), p.1223-1245, 2007Trabajos contenidos:

Lemanski, S.L
Nurick, G.N
Langdon, G.S
Simmons, M.C
Cantwell, W.J
Schleyer, G.K

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Resumen: 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.

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Item type	Current library	Collection	Call number	Status	Date due	Barcode
Documentos solicitados	CICY Documento préstamo interbibliotecario	Ref1	B-13140 (Browse shelf(Opens below))	Available

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.

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