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Molecular modelling of entangled polymer fluids under flow The ...

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3.2. SINGLE MODE POM-POM MODEL 51<br />

γ . [sec -1 ]<br />

0.25<br />

0.2<br />

1.225<br />

0.7<br />

3.0<br />

5.0<br />

0.25<br />

affine<br />

S xy<br />

0.15<br />

0.1<br />

0.05<br />

0<br />

0 5 10 15 20<br />

time [sec]<br />

Figure 3.1: Evolution <strong>of</strong> S xy for simple shear shear, ˙γ = 1sec −1 . Affine deformation<br />

corresponds to τ b = ∞ . <strong>The</strong> thin solid line corresponds to the value <strong>of</strong> τ b for which<br />

the steady state value <strong>of</strong> S xy is maximised.<br />

value <strong>of</strong> S xy can be shown to be<br />

τ b(max) =<br />

√<br />

3/2<br />

. (3.3)<br />

˙γ<br />

This is shown as the thin solid line in figure 3.1. <strong>The</strong> dashed curves in figure 3.1, which<br />

correspond to values <strong>of</strong> τ b other than τ b(max) , all fall below the τ b(max) curve in steady<br />

state. When τ b < τ b(max) the rapid reptation means that the <strong>flow</strong> is not fast enough,<br />

on average, to orientate the backbones significantly before they relax. For τ b > τ b(max)<br />

the backbones are orientated through the optimum angle but the <strong>flow</strong> then continues<br />

to orientate them towards the x-axis before the slow orientation relaxation produces<br />

a dynamic equilibrium.<br />

<strong>The</strong> contribution <strong>of</strong> a single backbone to S xy is maximised<br />

when it lies in the x-y plane, making an angle <strong>of</strong> 45 o with the x-axis. At this angle<br />

the contribution to S xy is 1/2. Note that even in the affine case S xy never reaches this<br />

value since, due to the isotropic initial distribution <strong>of</strong> backbones, all <strong>of</strong> the backbones<br />

will never simultaneously point in the same direction.<br />

For nearly exponential shear the full analytic solution for S xy is<br />

(1 + 2 α τ b ) ( e αt − 1 )<br />

S xy =<br />

),<br />

(6 ατ b + 2ατ b e 2αt + 2ατ b e − t<br />

τ b − 4ατ b e (α− 1 )t − τ b + 2e t<br />

τ b − 2e (α− 1 )t τ b + 9 +<br />

3<br />

ατ b<br />

(3.4)<br />

with α as defined in equation 3.1. Figure 3.2 shows plots <strong>of</strong> S xy for varying backbone<br />

orientation times. <strong>The</strong> solutions for S xy separate into two distinct regimes. For 1/τ b < α

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