Metal Foams: A Design Guide
Metal Foams: A Design Guide
Metal Foams: A Design Guide
- TAGS
- upload.vnuki.org
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⊳