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If the skins are peeled from the core, a sandwich structure loses its strength and stiffness. This can occur under - wave-slamming in fast ferries - rapid depressurisation of an aircraft The single cantilever beam (SCB) is used for thick-skinned structures. The lower skin is loaded forcing a crack along the skin-core interface. The force-displacement (P-δ) curve and crack lengths, a, are recorded The compliance, C, is assumed to follow:
Typical values:
Glass fibre epoxy/balsa 900 J/m2 Carbon fibre/PVC foam 2000 J/m2
how can you access the general purpose registers of Microprocessor in windows XP/2000/98...
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