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VDM-Based Remodeling 247<br />

6.4.3.3 Remodeling of Material Properties<br />

Modification of the element cross-section influences both its stiffness and mass at the same<br />

time. However, they are also related to the properties of the material, which is often modified<br />

directly by exchanging structural elements while retaining the same element cross-sections.<br />

In this case, the density and Young’s modulus modification parameters, μ ρ<br />

i and μE i ,haveto<br />

be used in Equations (41) instead of μA i . As be<strong>for</strong>e, the damping coefficients are assumed to<br />

remain constant, ˆαN = αN and ˆλi = λi; the variables are the densities ˆρl and Young’s moduli<br />

Êi of the elements of the modified structure. As in the previously considered case of material<br />

redistribution, all four virtual distortions are nonvanishing and the general <strong>for</strong>m of the system<br />

of Equation (43) is retained, besides the same minor computational simplifications, which are<br />

related to the fact that (αM)NM = αN MNM and (λS)ii = λiSii. The response of the<br />

modified structure can be computed by solving the general system and by substituting the<br />

resulting virtual distortions into Equations (42).<br />

Differentiations of Equations (41) with respect to the densities and Young’s moduli of the<br />

elements of the modified structure yield<br />

∂MNM<br />

∂ ˆρl<br />

∂ (αM) NM<br />

∂ ˆρl<br />

∂ (λS) ii<br />

∂ ˆρl<br />

= Ml<br />

NM<br />

= αN<br />

ˆρl<br />

= ∂Sii<br />

∂ ˆρl<br />

,<br />

M l<br />

NM<br />

ˆρl<br />

= 0,<br />

∂MNM<br />

∂ Êl<br />

∂ (λS) ii<br />

∂ Êl<br />

∂Sii<br />

∂ Êl<br />

= ∂ (αM) NM<br />

∂ Êl<br />

= δilλi Ai<br />

= δil Ai<br />

Differentiations of the original system of Equation (43) yield the two following linear systems:<br />

F ω<br />

⎡<br />

∂ f<br />

⎢<br />

⎣<br />

0 K<br />

∂ ˆρl<br />

∂d 0 K<br />

∂ ˆρl<br />

∂φ0 ⎤<br />

⎥ ⎡<br />

⎥<br />

2 ∂MNM<br />

⎥ ⎢<br />

ω<br />

⎥ ⎢ ∂ ˆρl<br />

⎥ ⎢<br />

⎥ ⎢<br />

⎥ = ⎢−iω<br />

⎥ ⎢<br />

k ⎥ ⎢<br />

∂<br />

⎥ ⎣<br />

ˆρl ⎥<br />

⎦<br />

∂ (αM) NM<br />

∂ ˆρl<br />

0<br />

0<br />

∂ε 0 k<br />

∂ ˆρl<br />

u M<br />

u M<br />

= 0<br />

⎤<br />

⎥ , F<br />

⎥<br />

⎦<br />

ω<br />

⎡<br />

∂ f<br />

⎢<br />

⎣<br />

0 K<br />

∂ Êl<br />

∂d 0 K<br />

∂ Êl<br />

∂φ0 ⎤<br />

⎥ ⎡<br />

⎥<br />

0<br />

⎥ ⎢<br />

⎥ ⎢ 0<br />

⎥ ⎢<br />

⎥ ⎢<br />

⎥ = ⎢−iω<br />

⎥ ⎢<br />

k ⎥ ⎢<br />

⎥<br />

∂<br />

⎣<br />

Êl ⎥<br />

⎦<br />

∂ (λS) ii<br />

∂ Êl<br />

− ∂Sii<br />

εi<br />

∂ Êl<br />

which, after substitution of Equations (47), can be used to obtain the derivatives of the virtual<br />

distortions and, by Equations (44), yield the derivatives of the response.<br />

References<br />

1. N. Kikuchi and M. P. Bendsøe, Generating optimal topologies in structural design using homogenization<br />

method, Computer Methods in Applied Mechanics and Engineering, 71(2), November<br />

1988, 197–224.<br />

2. A. R. Diaz and M. P. Bendsøe, Shape optimization of multipurpose structures by homogenization<br />

method, Structural Optimization, 4, 1992, 17–22.<br />

∂ε 0 k<br />

∂ Êl<br />

εi<br />

⎤<br />

⎥<br />

⎦<br />

(47)

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