12.02.2013 Views

Metal Foams: A Design Guide

Metal Foams: A Design Guide

Metal Foams: A Design Guide

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

58 <strong>Metal</strong> <strong>Foams</strong>: A <strong>Design</strong> <strong>Guide</strong><br />

(i) Write down an equation for the objective<br />

(ii) Eliminate the free variable(s) in this equation by using the constraints<br />

(iii) Read off the grouping of material properties (called the material index)<br />

which maximize or minimize the objective.<br />

A more detailed recipe is given in Table 5.2. Indices for numerous standard<br />

specifications are listed in the Appendix at the end of this <strong>Design</strong> <strong>Guide</strong>.<br />

5.3 Two examples of single-objective optimization<br />

Panel of specified stiffness and minimum mass<br />

The mode of loading which most commonly dominates in engineering is not<br />

tension, but bending. Consider the performance metric for a panel of specified<br />

length, ℓ, and width, b (Figure 5.1), and specified stiffness, with the objective<br />

of minimizing its mass, m. Themassis<br />

t<br />

m D bt ⊲5.1⊳<br />

l<br />

F/unit width<br />

Figure 5.1 A panel of length, ℓ, width, b, and thickness, t, loaded in<br />

bending by a force, F, per unit width<br />

where t is the thickness of the panel and is the density of the material of<br />

which it is made. The length, ℓ, width, b, and force, F, per unit width are<br />

specified; the thickness, t, is free. We can reduce the mass by reducing t, but<br />

there is a lower limit set by the requirement that the panel must meet the<br />

constraint on its bending stiffness, S, meaning that it must not deflect more<br />

than υ under a load Fb. To achieve this we require that<br />

S D Fb<br />

υ<br />

B1EI<br />

D ½ SŁ<br />

3<br />

ℓ<br />

b<br />

⊲5.2⊳<br />

where S Ł is the desired bending stiffness, E is Young’s modulus, B1 is a<br />

constant which depends on the distribution of load (tabulated in Chapter 6,<br />

Section 6.3) and I is the second moment of the area of the section. This, for<br />

a panel of section b ð t, is<br />

I D bt3<br />

12<br />

⊲5.3⊳

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!