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Metal Foams: A Design Guide

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Cost estimation and viability 215<br />

Conventional alloys (cast irons, steels, aluminum alloys) lie in the lower part<br />

of the diagram. Beryllium alloys, CFRPs and Al-based MMCs lie in the central<br />

and upper parts.<br />

The trade-off surface for conventional, fully dense, materials is shown by<br />

the shaded band. <strong>Metal</strong> foams lie in the unpopulated sector of the diagram – all<br />

three classes of foam offer non-dominated solutions to this problem. But even<br />

so, they are viable only if the mass/value exchange constant lies in the right<br />

range. To explore this question for the panel of specified stiffness we define<br />

the value function<br />

�<br />

V D ˛1P1 C ˛2P2 D ˛1<br />

E 1/3<br />

� �<br />

C<br />

C<br />

E 1/3<br />

�<br />

⊲16.16⊳<br />

(since ˛2, relating value to cost, is unity). Values of ˛1, relating value to<br />

mass, are listed in Table 16.2. The equation is evaluated in Table 16.3 for<br />

two extreme values of ˛1 for a set of materials including cast irons, steels,<br />

aluminum alloys, titanium, beryllium and three metal foams. When ˛1 has the<br />

low value of 0.5£/kg, nodular cast irons are the best choice. But if ˛1 is as<br />

Table 16.3 The selection of panel materials: stiffness constraint<br />

Material E Cm P1 P2 V V<br />

Mg/m 3 GPa £/kg ˛1 D ˛1 D<br />

£0.5/kg £500/kg<br />

Cast iron,<br />

nodular<br />

7.30 175 0.25 1.31 0.33 0.99 655<br />

Low-alloy<br />

steel (4340)<br />

7.85 210 0.45 1.32 0.59 1.25 660<br />

Al-6061-T6 2.85 70 0.95 0.69 0.66 1.01 345<br />

Al-061–20%<br />

SiC, PM<br />

2.77 102 25 0.59 14.8 15.1 309<br />

Ti-6-4 B265<br />

grade 5<br />

4.43 115 20 0.91 18.2 18.7 473<br />

Beryllium<br />

SR-200<br />

1.84 305 250 0.27 67.5 67.6 202<br />

Alporasa 0.25 1.0 40 0.23 10.0 10.1 125<br />

Alulighta 0.30 0.8 16 0.3 5.2 5.4 155<br />

Alcana 0.25 0.4 5.8 0.34 2.0 2.2 172<br />

a All three types of metal foam are made in a range of densities, with a corresponding range of properties. These three examples<br />

are taken from the middle of the ranges. The costs are estimates only, broadly typical of current prices, but certain to change<br />

in the future. It is anticipated that large-scale production could lead to substantially lower costs.

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