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A Brief Review of Elasticity and Viscoelasticity for Solids 1 Introduction

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28 H. T. Banks, S. H. Hu <strong>and</strong> Z. R. Kenz / Adv. Appl. Math. Mech., 3 (2011), pp. 1-51<br />

where H(t) is the Heaviside step function (also called the unit step function in the literature),<br />

t 0 ≥ 0. The solution σ(t) to (3.16) is the relaxation function. With this strain<br />

function, (3.16) can be written as<br />

where δ is the Dirac delta function. Let<br />

σ<br />

η + 1 dσ<br />

κ dt = ε 0δ(t − t 0 ),<br />

ˆσ(s) = L {σ(t)}(s),<br />

where L denotes the Laplace trans<strong>for</strong>m. Then taking the Laplace trans<strong>for</strong>m <strong>of</strong> both<br />

sides <strong>of</strong> the above differential equation we obtain<br />

(<br />

ˆσ(s) = ε 0 e −t 1<br />

0s<br />

η + 1 ) −1 (<br />

κ s = κε0 e −t 0s<br />

s + κ ) −1.<br />

η<br />

Taking the inverse Laplace trans<strong>for</strong>m one finds that<br />

[<br />

σ(t) = κ exp − κ ]<br />

η (t − t 0) ε 0 H(t − t 0 ).<br />

The stress relaxation function <strong>for</strong> the Maxwell model (3.16) is illustrated in Fig. 9 (compare<br />

with Fig. 4).<br />

The creep function corresponds to the creep that occurs under the imposition <strong>of</strong> a<br />

constant stress given by<br />

σ(t) = σ 0 H(t − t 0 ), <strong>and</strong> ε(0) = 0,<br />

the solution ε(t) to (3.16) is the creep function. With this stress function, (3.16) can be<br />

written as<br />

dε<br />

dt = σ 0<br />

η H(t − t 0) + σ 0<br />

κ δ(t − t 0).<br />

Then taking the Laplace trans<strong>for</strong>m <strong>of</strong> both sides <strong>of</strong> the above differential equation we<br />

have that<br />

ˆε(s) = σ 0<br />

η<br />

e −t 0s<br />

s 2 + σ 0<br />

κ<br />

Upon taking the inverse Laplace trans<strong>for</strong>m we find<br />

ε(t) =<br />

e −t 0s<br />

[ 1<br />

κ + 1 η (t − t 0)]<br />

σ 0 H(t − t 0 ).<br />

The creep function <strong>of</strong> Maxwell model (3.16) is illustrated in Fig. 10 (again, compare<br />

with Fig. 5).<br />

s<br />

.

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