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.

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

A thin-walled elastic tube will buckle inwards under an external pressure<br />

p 0 , given in the last box. Here I refers to the second moment of area of a<br />

section of the tube wall cut parallel to the tube axis.<br />

(b) <strong>Metal</strong> foams<br />

The moduli of open-cell metal foams scale as ⊲ / s⊳ 2 , that of closed-cell<br />

foams has an additional linear term (Table 4.2). When seeking elastic-buckling<br />

resistance at low weight, the material index characterizing performance (see<br />

Appendix) is E 1/2 / (beams) or E 1/3 / (panels). As beam-columns, foams<br />

have the same index value as the material of which they are made; as<br />

panels, they have a higher one, meaning that the foam panel is potentially<br />

lighter for the same buckling resistance. Sandwich structures with foam cores<br />

(Chapter 10) are better still. Clamping metal foams requires special attention:<br />

see Section 6.7.<br />

6.6 Torsion of shafts<br />

(a) Isotropic solids<br />

A torque, T, applied to the ends of an isotropic bar of uniform section, and<br />

acting in the plane normal to the axis of the bar, produces an angle of twist<br />

. The twist is related to the torque by the first equation below, in which<br />

G is the shear modulus. For round bars and tubes of circular section, the<br />

factor K is equal to J, the polar moment of inertia of the section, defined in<br />

Section 6.2. For any other section shape K is less than J. ValuesofK are<br />

given in Section 6.2.<br />

If the bar ceases to deform elastically, it is said to have failed. This will<br />

happen if the maximum surface stress exceeds either the yield strength, y, of<br />

the material or the stress at which it fractures. For circular sections, the shear<br />

stress at any point a distance r from the axis of rotation is<br />

D Tr<br />

K D G r<br />

ℓ<br />

The maximum shear stress, max, and the maximum tensile stress, max, are<br />

at the surface and have the values<br />

max D max D Td0<br />

2K<br />

D G d0<br />

2ℓ<br />

If max exceeds y/2 (using a Tresca yield criterion), or if max exceeds the<br />

MOR, the bar fails, as shown in Figure 6.5. The maximum surface stress<br />

for the solid ellipsoidal, square, rectangular and triangular sections is at the

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

Saved successfully!

Ooh no, something went wrong!