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Metal Foams: A Design Guide

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c<br />

t<br />

p<br />

p<br />

Figure 10.9 Sandwich panel under uniform load<br />

b<br />

Sandwich structures 127<br />

effect of different core densities. The objective is to choose the thickness of the<br />

core, c, and the thickness of each of the two face sheets, t, so as to minimize<br />

the weight of the plate. The width of the plate is assumed large compared<br />

with ℓ and the design exercise focuses on a one dimensional, wide plate.<br />

Deflection and failure constraints<br />

The first step in the optimization process is identification of the constraints on<br />

failure and deflection. For the sandwich plate under uniform transverse pressure,<br />

face sheet yielding and wrinkling must be considered, as well as yielding<br />

of the core (Figure 10.10). Deflection constraints must also be imposed to<br />

ensure that deflections of an optimally designed panel do not exceed tolerable<br />

limits. Normal crushing (indentation) of the core will not be at issue<br />

because the loading pressure, p, will necessarily be small compared with the<br />

compressive yield strength of the core material.<br />

In the example considered, the face sheet material is the same as that of the<br />

fully dense core material (i.e. s D f, s y D f y and Es D Ef). The relation<br />

between the core modulus and density is taken to be<br />

Ec/Es D ˛2⊲ c/ s⊳ 2<br />

⊲10.22a⊳<br />

where ˛2 is a quality factor, with ˛2 D 1 applying to a core material having<br />

relatively inferior properties and ˛2 D 4 to a material with properties somewhat<br />

higher than those currently available. The core is assumed to be isotropic with

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