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Metal Foams: A Design Guide

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Indentation<br />

Sandwich structures 117<br />

The indentation mode of collapse involves the formation of four plastic hinges<br />

within the top face sheet adjacent to each indenter, with compressive yield of<br />

the underlying core, as sketched in Figure 10.3. Early studies on the indentation<br />

of polymer foams (for example, Wilsea et al., 1975) and more recently<br />

on metal foams (Andrews et al., 1999) reveal that the indentation pressure is<br />

only slightly greater than the uniaxial compressive strength. The underlying<br />

cause of this behavior is the feature that foams compress with little transverse<br />

expansion (see Chapter 7 and Gibson and Ashby, 1997).<br />

Plastic hinge<br />

F/2<br />

F<br />

a ;;<br />

λ ;; q<br />

;;<br />

;;<br />

s C Y<br />

M p<br />

Figure 10.3 Indentation mode of collapse for a three-point bend<br />

configuration<br />

F/2<br />

Consider first the case of three-point bending. Then the collapse load F on<br />

the upper indenter can be derived by a simple upper bound calculation. Two<br />

segments of the upper face, of wavelength , are rotated through a small angle<br />

. The resulting collapse load is given by<br />

F D 4Mp C ⊲a C ⊳ b c y ⊲10.12⊳<br />

where Mp D bt2 /4 is the full plastic moment of the face-sheet section. Minimization<br />

of this upper bound solution for F with respect to the free parameter<br />

gives an indentation load FI of<br />

FI D 2bt<br />

� cy<br />

and a wavelength<br />

�<br />

�<br />

�<br />

D t�<br />

f y<br />

c<br />

y<br />

f<br />

y C ab c y<br />

⊲10.13⊳<br />

⊲10.14⊳<br />

We note in passing that the same expression for FI and as given by<br />

equations (10.13) and (10.14) are obtained by a lower bound calculation, by

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