WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...
WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...
WAVES AND VIBRATIONS IN INHOMOGENEOUS STRUCTURES ...
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896 S. Halkjær, O. Sigmund and J. S. Jensen<br />
distributions. The design variables are spatial material densities.<br />
By using analytical sensitivity analysis and mathematical<br />
programming tools it is possible efficiently to handle<br />
a large number of design variables. We base our<br />
implementation on Finite Element (FE) modelling and typically<br />
choose one continuous design variable per element<br />
or node:<br />
z e 2 R ; e ¼ 1; ...; N ; ð1Þ<br />
where N is the number of finite elements or nodes in the<br />
design domain. It should be emphasized that the method<br />
can be used with a finite difference discretization just as<br />
easily and that more design variables can be assigned to<br />
each element in order to distribute more than two materials<br />
in the design domain.<br />
The goal for the optimization algorithm is to distribute<br />
two materials in a domain such that some cost function is<br />
minimized (or maximized). The continuous design variables<br />
control the material distribution by defining the element-wise<br />
constant material properties in each element. If<br />
r e denotes an element-wise property we can write:<br />
r e ¼ð1 z eÞ r 1 þ r 2 z e ð2Þ<br />
where subscript 1 and 2 refers to the properties of material<br />
1 and material 2, respectively. In this case we let z e vary<br />
continuously between 0 and 1, such that for z e ¼ 0 the<br />
corresponding element takes the material properties of material<br />
1 and for z e ¼ 1 those of material 2.<br />
Denoting the cost function F we can now formulate<br />
the optimization problem as follows:<br />
min:<br />
F ¼ Fðw; u; zÞ ; ð3Þ<br />
z<br />
s:t:: giðzÞ g* i ; ð4Þ<br />
0 ze 1 ; e ¼ 1; ...; N ; ð5Þ<br />
ðK w 2 MÞ u ¼ f ; ð6Þ<br />
where Eq. (6) is the discretized FE equation of the timeharmonic<br />
wave propagation problem. The vector u contains<br />
the discretized nodal values of the complex amplitudes<br />
of the displacement field, and K and M are the stiffness<br />
and mass matrices, respectively. The load vector f<br />
comes from external wave loading. In (4) a number of<br />
additional constraints can be specified, e.g. specifying a<br />
maximum amount of a single material component. For<br />
more details about computational procedures, sensitivity<br />
analysis and more, the reader is referred to [2].<br />
The advantage of using continuous design variables is<br />
that it allows for the use of efficient gradient-based optimization<br />
algorithms. However, it also implies that we may<br />
end up with values of z e that are neither 0 or 1, but an<br />
intermediate value that does not correspond to any of the<br />
two materials. There are several ways to penalize the appearance<br />
of intermediate density solutions (see e.g. [2]),<br />
however, it is our experience that intermediate densities<br />
seldomly remain in the optimized band gap designs since<br />
band gaps are favoured by maximum contrast in the material<br />
properties. Therefore we have not used any penalization<br />
techniques in this work.<br />
As for all topology optimization problems with spatial<br />
material distribution the results depend on the mesh. How-<br />
ever, as opposed to conventional stiffness design problems<br />
where the objective is improved with mesh-refinement, it<br />
appears that the finite length of the elastic waves imposes<br />
a length-scale for the present band gap design problems<br />
and thus we do usually not experience a significant meshdependence.<br />
Therefore, we do not use regularization techniques<br />
in this paper. For more discussions of this issue,<br />
the reader is referred to [2]. Concerning the convergence<br />
of the finite element model, we require discretizations that<br />
at least have 10 elements pr. wave-length. Due to the reasons<br />
discussed above, we do not expect to find significantly<br />
different design solutions if the mesh is further refined.<br />
Design of 1D structures:<br />
the infinite periodic elastic beam<br />
In this section, we study elastic wave propagation in a<br />
periodic beam of infinite length. The beam consists of an<br />
infinite number of copies of a base cell with a specific<br />
geometry and material distribution. The periodicity introduces<br />
frequency band gaps for both longitudinal and bending<br />
waves, preventing waves with frequencies in these<br />
gaps from propagating in the beam. In general, the band<br />
gap frequency ranges for the two wave types are different,<br />
but for certain geometries and material distributions of the<br />
base cell, band gaps for the two wave types overlap, preventing<br />
both of the two wave types from propagating in<br />
the beam. Such studies are relevant in design problems<br />
where vibration insulation and filtering are important objectives.<br />
Theory<br />
Let the beam axis be directed along the x-axis. Longitudinal<br />
wave propagation in the beam is described using the<br />
usual 1D theory<br />
@<br />
@x<br />
@u<br />
E<br />
@x ¼ q @2u @t2 ð7Þ<br />
where u ¼ uðx; tÞ denotes the displacement along the x-axis.<br />
q denotes the mass density and E is Young’s modulus.<br />
Bending waves in the beam are described by Timoshenko<br />
theory<br />
@<br />
@x<br />
@<br />
@x<br />
ksGA @w<br />
@x þ q ¼ qA @2w ; ð8Þ<br />
@t2 EI @q<br />
@x<br />
ksGA @w<br />
@x þ q ¼ qI @2q @t2 ð9Þ<br />
where w ¼ wðx; tÞ and q ¼ qðx; tÞ denote the transverse<br />
displacement and angle of rotation of the cross-section respectively.<br />
A, I, G and ks denote the cross-sectional area,<br />
area moment of inertia, shear modulus and the shear correction<br />
coefficient, respectively. Here, we use<br />
ks ¼ 6ð1 þ nÞ=ð7 þ 6nÞ [14] for a circular cross-section,<br />
where n is the Poisson ratio. Timoshenko theory is used,<br />
as the ratio between considered wave length and cross-section<br />
dimension is smaller than the lower bound ( 20) for<br />
using the simpler Bernoulli-Euler theory.