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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
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Variable magnetic coupling transducers A transducer of this type relies on variable coupling between magnetic coils. An example is a Linear Variable Differential Transformer (L
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Flow at low Mach number and zero incidence about M6 wing Results from FP were obtained corresponding to M ∞ = 0.2 and a = 0 and, as noted, with the input files generated by FP
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