Metal Foams: A Design Guide
Metal Foams: A Design Guide
Metal Foams: A Design Guide
- TAGS
- upload.vnuki.org
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
where<br />
D<br />
�<br />
2⊲1<br />
Eft<br />
2 f ⊳GcR<br />
Sandwich structures 141<br />
⊲10.45b⊳<br />
Here, R is the shell radius, t the face sheet thickness, c the core thickness.<br />
The parameter measures the relative shear compliance of the core. It must<br />
be less than 1/ p 2 to avoid localized shear kinking of the shell wall. This<br />
result (10.45) applies if the length of the shell ℓ is at least several times the<br />
axial buckle wavelength. It also assumes that sufficiently strong end support<br />
conditions are in effect. End conditions modify (10.45) slightly, but not as<br />
much as imperfections, to be discussed later.<br />
The condition for face yielding of the perfect shell prior to (or simultaneous<br />
with) buckling is:<br />
N D 2t f y<br />
⊲10.46⊳<br />
Yielding of the core does not directly affect the load-carrying capacity since<br />
it supports no significant load. However, it will affect the ability of the core to<br />
suppress face sheet wrinkling and to maintain the shear stiffness necessary for<br />
post-buckling load-carrying capacity. Yielding of the core prior to buckling<br />
is avoided if the axial strain in the unbuckled shell (ε D N/⊲2tEf⊳) does not<br />
exceed the uniaxial compressive yield strain of the core. In other words, core<br />
yielding is excluded if its yield strain is larger than that of the face sheets.<br />
If neither the core nor the face sheets yield, face sheet wrinkling may occur.<br />
It is governed by the condition introduced earlier (equation (10.24b)). In terms<br />
of the load per unit circumferential length, the onset of face sheet wrinkling<br />
in the perfect shell occurs when<br />
N D 2tk⊲EfE 2 c ⊳1/3<br />
⊲10.47⊳<br />
For shells with core parent material identical to the face sheet material<br />
( s D f and Ef D Es), with core modulus and density still related by<br />
equation (10.22a), the weight index is<br />
D<br />
W<br />
2 R 2 ℓ f<br />
D 2 t c c<br />
C<br />
R s R<br />
⊲10.48⊳<br />
When the shell buckles elastically, uninfluenced by yielding or wrinkling,<br />
global optimization of the shell could be carried out analytically to obtain the<br />
values of t, c and c which minimize the weight of the shell for prescribed<br />
N. This elastic optimization implies that the core weight is twice that of the<br />
two face sheets. However, it is of little practical value because face sheet<br />
yielding or wrinkling invariably intervene at the levels of load index wherein<br />
the sandwich shell is weight competitive.