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Metal Foams: A Design Guide

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where<br />

D<br />

�<br />

2⊲1<br />

Eft<br />

2 f ⊳GcR<br />

Sandwich structures 141<br />

⊲10.45b⊳<br />

Here, R is the shell radius, t the face sheet thickness, c the core thickness.<br />

The parameter measures the relative shear compliance of the core. It must<br />

be less than 1/ p 2 to avoid localized shear kinking of the shell wall. This<br />

result (10.45) applies if the length of the shell ℓ is at least several times the<br />

axial buckle wavelength. It also assumes that sufficiently strong end support<br />

conditions are in effect. End conditions modify (10.45) slightly, but not as<br />

much as imperfections, to be discussed later.<br />

The condition for face yielding of the perfect shell prior to (or simultaneous<br />

with) buckling is:<br />

N D 2t f y<br />

⊲10.46⊳<br />

Yielding of the core does not directly affect the load-carrying capacity since<br />

it supports no significant load. However, it will affect the ability of the core to<br />

suppress face sheet wrinkling and to maintain the shear stiffness necessary for<br />

post-buckling load-carrying capacity. Yielding of the core prior to buckling<br />

is avoided if the axial strain in the unbuckled shell (ε D N/⊲2tEf⊳) does not<br />

exceed the uniaxial compressive yield strain of the core. In other words, core<br />

yielding is excluded if its yield strain is larger than that of the face sheets.<br />

If neither the core nor the face sheets yield, face sheet wrinkling may occur.<br />

It is governed by the condition introduced earlier (equation (10.24b)). In terms<br />

of the load per unit circumferential length, the onset of face sheet wrinkling<br />

in the perfect shell occurs when<br />

N D 2tk⊲EfE 2 c ⊳1/3<br />

⊲10.47⊳<br />

For shells with core parent material identical to the face sheet material<br />

( s D f and Ef D Es), with core modulus and density still related by<br />

equation (10.22a), the weight index is<br />

D<br />

W<br />

2 R 2 ℓ f<br />

D 2 t c c<br />

C<br />

R s R<br />

⊲10.48⊳<br />

When the shell buckles elastically, uninfluenced by yielding or wrinkling,<br />

global optimization of the shell could be carried out analytically to obtain the<br />

values of t, c and c which minimize the weight of the shell for prescribed<br />

N. This elastic optimization implies that the core weight is twice that of the<br />

two face sheets. However, it is of little practical value because face sheet<br />

yielding or wrinkling invariably intervene at the levels of load index wherein<br />

the sandwich shell is weight competitive.

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