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5 Linear Viscoelasticity

The main goal of this Chapter is to answer the questions:

In the lecture, several examples of elastic, viscous, and viscoelastic materials are discussed. For example, we perceive a rubber (elastomer) as a prototypical elastic material, since after loading and subsequent unloading the material attains its original shape (memo: “rubber bands”). Furthermore, we expect that an elastic material shows a stress-strain response that is independent of the applied rate of deformation. The other extreme is a viscous material. If it is loaded and subsequently unloaded, the final shape differs significantly from its original one, and also do the stresses during deformation depend on the rate of deformation, rather on the deformation itself. The third category of materials, viscoelastic, shows a behavior that is between that of elastic and viscous ones. In order to discuss this in detail, we limit ourselves first to the case of linear viscoelasticity.

Also, we restrict our attention in this Chapter to the 1-dimensional case.

For some examples for non-elastic material behavior, see:

Amazing material - no gimmicks! (jabbaboy)

Body Armour Tested With Various Guns Including An Uzi And A Magnum (InterconnectiveLtd)

Three Viscoelastic Effects (psidot)

5.1Starting point: Hookean solid

A purely linear elastic material in 1D can be described by the following stress-strain relation,

σ=G γ ,\psigma = G \ \gstrn \ ,

which is a Hooke-type relation between the stress σ\psigma and the shear strain γ\gstrn, with shear modulus GG. We note in passing that this stress-strain relation can also be expressed as a derivative of a free energy density AA,

σ=∂A(γ)∂γ ,\psigma = \frac{\partial A(\gstrn)}{\partial \gstrn} \ ,

with the help of A=(G/2)γ2A = (G/2) \gstrn^2. It is manifest that in such (elastic) systems, the stress state depends only on the current strain, irrespective of the deformation history. In other words,

but rather it is only affected by the current state of deformation, by the current value of γ\gstrn.

Rate-independence of elastic deformation.

Figure 5.1:Rate-independence of elastic deformation.

One can ask the question how much work is done on a mechanical system that is deformed over time. Specifically, if a system is deformed with a certain (time-variable) strain rate γ˙(t)\dot{\gstrn}(t) from time t1t_1 until t2t_2, then the work done ΔW\Delta W on the system is equal to

ΔW=∫t1t2σ(γ(t)) γ˙(t) dt .\Delta W = \int^{t_2}_{t_1} \psigma(\gstrn(t)) \ \dot{\gstrn}(t) \ dt \ .

If we use the fact that the stress σ\psigma depends only on the actual strain γ(t)\gstrn(t), and since γ˙=dγ/dt\dot{\gstrn} = d\gstrn/dt, one can substitute integration variables from time tt to strain γ\gstrn, to obtain the work done in terms of a strain-integral,

ΔW=∫γ(t1)γ(t2)σ(γ) dγ .\Delta W = \int^{\gstrn(t_2)}_{\gstrn(t_1)} \sigma(\gstrn) \ d\gstrn \ .

If we now use the hyperelasticity relation (5.2), one finds

ΔW=∫γ(t1)γ(t2)σ(γ) dγ=∫γ(t1)γ(t2)∂A(γ)∂γ dγ=A(γ(t2))−A(γ(t1)) .\Delta W = \int^{\gstrn(t_2)}_{\gstrn(t_1)} \sigma(\gstrn) \ d\gstrn =\int^{\gstrn(t_2)}_{\gstrn(t_1)} \frac{\partial A(\gstrn)}{\partial \gstrn} \ d\gstrn = A(\gstrn(t_2))-A(\gstrn(t_1)) \ .

In other words, the work done on the system is given by the free energy difference between final and initial state. This implies particularly, that there is no work done after a complete cycle of deformation, since in this case γ(t2)=γ(t1)\gstrn(t_2)=\gstrn(t_1) and therefore also A(γ(t2))=A(γ(t1))A(\gstrn(t_2))=A(\gstrn(t_1)).

5.2Standard measurement protocols

We have seen that an ideal elastic solid shows a mechanical behavior that is completely path-independent. If the material is loaded over time, the current stress state depends only on the current strain. This is different for all other than purely elastic materials, and it hence makes sense to define some characteristic measurements, under which the mechanical behavior can be tested. There is a number of standard measurement protocols, namely:

Standard measurement protocols: (a) step-strain, (b) step-strain rate, (c) (sinusoidal) oscillation, and (d) creep.

Figure 5.2:Standard measurement protocols: (a) step-strain, (b) step-strain rate, (c) (sinusoidal) oscillation, and (d) creep.

In order to get a feeling for these four standard measurement protocols, the reader is encouraged to draw quantitatively the material response for the two extreme cases, namely

5.3Origin of viscoelasticity, time scales

Imposing deformation on a piece of material brings the material away from its equilibrium state. This can be observed on the macroscopic scale by the emergence of stresses. On the microscopic scale, each constituent particle (atom, monomer, ...) is not anymore in a state of balanced-forces, and hence the deformation results on small scales to unbalanced forces. These unbalanced forces on the microscopic scale and the stresses on the macroscopic scale are different languages to describe one and the same situation: a material is deformed away from its equilibrium shape.

Immediately after imposing the deformation, there are stresses in the material. The question is now what happens with these stresses if the deformation is maintained. Sloppily speaking, materials do not like to be in a stressed state (thermodynamics allows to make more precise statements about this), and if the material has any means to relax the current stress, it will do so. However, how can a material relax stress, while the imposed deformation is maintained? This happens by way of internal relaxation processes. Structural rearrangements occur on the microscopic scale such that the constituent particles evolve towards a configuration/state in which force balance is again respected; that latter state will be observed macroscopically as a state with vanishing stress. Making these necessary structural rearrangements is a dynamic process, and it does thus not come as a surprise that one can associate a characteristic time scale with that process, called relaxation time scale τrelax\taur.

Based on the existence of a relaxation time scale τrelax\taur, one can now discuss what happens when, for example, the imposed rate of deformation γ˙\dot{\gstrn} is much larger or much smaller than the rate for internal structural relaxation, τrelax−1\taur^{-1}:

It is clear from the above, that a material with internal time scale τrelax\taur shows both elastic as well as viscous deformation characteristics if it is deformed at an intermediate rate γ˙≃τrelax−1\dot{\gstrn} \simeq \taur^{-1}, in other words γ˙ τrelax≃1\dot{\gstrn} \ \taur \simeq 1.

In summary, the characteristic response of the material depends on the ratio of the applied rate of deformation to the internal rate of structural relaxation. For that purpose, it is customary to use the so-called Weissenberg number, defined as

We=γ˙ τrelax ,{\rm We} = \dot{\gstrn} \ \taur \ ,

which is a useful dimensionless quantity for discussing viscoelastic phenomena.

Typical time scales do not only occur in classical materials, but they can also be observed in “crowd dynamics”:

Aggregate Dynamics for Dense Crowd Simulation (GAMMA UMD)

5.4Maxwell element

5.4.1Basics, definition

A useful tool for describing the behavior of materials with both elastic and viscous behavior is to use a combination of the two extremes, which are here summarized again for convenience, in slightly adapted notation:

σ=G γHooke ,\psigma = G \ \gstrn_{\rm Hooke} \ ,
σ=η γ˙Newton .\psigma = \eta \ \dot{\gstrn}_{\rm Newton} \ .

Particularly, to mimic the behavior discussed in the previous section, we couple the two elements in series (see Figure 5.3), which is then called a Maxwell element. Since they are coupled in series, this implies that the strains and in particular also the strain rates can be added,

γ˙=γ˙Hooke+γ˙Newton .\dot{\gstrn} = \dot{\gstrn}_{\rm Hooke} + \dot{\gstrn}_{\rm Newton} \ .

With the help of (5.8) and (5.9) this can be cast into the form

γ˙=σ˙G+ση ,\dot{\gstrn} = \frac{\dot{\psigma}}{G} + \frac{\psigma}{\eta} \ ,

which is a 1st1^{\rm st}-order differential equation for the stress σ\psigma. The latter can be written is a more intuitive form:

σ˙=Gγ˙−τ−1σ ,\dot{\psigma}= G \dot{\gstrn} - \tau^{-1} \psigma \ ,

with the characteristic time scale

τ=ηG .\tau = \frac{\eta}{G} \ .

Since η\eta has units of [Pa s] and GG has units of [Pa], τ\tau is indeed a time scale. This time scale plays the role of τrelax\taur used in the previous section. However, since in this section we do not make explicit reference to the microscopic structural relaxation processes, we will simply use τ\tau in relation with the Maxwell element.

Maxwell element: Serial coupling of a spring and a dashpot.

Figure 5.3:Maxwell element: Serial coupling of a spring and a dashpot.

It is instructive to discuss the Maxwell model (5.12), before solving it in concrete cases. First, it is apparent that, if the first term on the right hand side was neglected, (5.12) is a simple relaxation equation with relaxation time τ\tau. Second, if all terms are taken into account and considering a constant deformation rate γ˙\dot{\gstrn}, the stationary state (σ˙=0\dot{\psigma}=0) is given by σ=η γ˙\psigma = \eta \ \dot{\gstrn}. Third if the viscosity is infinitely high (η→∞\eta \to \infty, representative of no structural relaxation), one finds σ˙=Gγ˙\dot{\psigma}= G \dot{\gstrn}, which represents the Hookean limit.

In other words, the serial coupling of a Hookean (elastic) and a Newtonian (viscous) element shows many features discussed above. In order to more precisely quantify the viscoelastic behavior of the Maxwell element defined in (5.12), one needs to perform the standard measurements discussed in Section 5.2: Strep-strain, step-strain rate, (sinusoidal) oscillation, and creep. This will be discussed further below in Section 5.4.3.

5.4.2Relaxation modulus

It can be shown[1] that the solution to the Maxwell model (5.12) can be written in the form

σ(t)=∫−∞tG(t−t′) γ˙(t′) dt′ ,\psigma(t) = \int^t_{-\infty} G(t-t') \ \dot{\gstrn}(t') \ dt' \ ,

with the relaxation modulus defined by

G(t−t′)=G exp⁡(−t−t′τ) .G(t-t') = G \ \exp\left(-\frac{t-t'}{\tau}\right) \ .
Boltzmann integral: Current stress as a weighted superposition of previous strain-states.

Figure 5.4:Boltzmann integral: Current stress as a weighted superposition of previous strain-states.

The explicit solution in the form (5.14) is called a Boltzmann integral. It shows the following features, see also Figure 5.4. First, it shows that the current stress state σ(t)\psigma(t) is a sum (integral) of effects of the strain rate γ˙(t′)\dot{\gstrn}(t') in the past (t′<tt' < t). Second, the strain-rate contribution at an earlier instant t′t' gets weighted by the factor G(t−t′)G(t-t') (which itself is a decreasing function of t−t′t-t'). Therefore, the further back t′t', the less does the strain rate γ˙(t′)\dot{\gstrn}(t') at that moment contribute to the current stress state. This is also in agreement with intuition, saying that there is an effect of fading memory: “the most recent deformation is most relevant, while the earlier deformations are less relevant for the current stress state”. Thirdly, (5.14) also shows that the current stress state depends linearly on the deformation. In other words, doubling the the rate of deformation at all times, leads to a doubling of the stress value. Because of all these features, (5.14) is one of the most important relations in linear viscoelasticity.

5.4.3Standard measurements

Earlier, the four standard measurement protocols have been discussed. We leave it to the reader to examine the behavior of the Maxwell model in a step-strain and in a step-strain rate experiment. However, we want to discuss here the cases of creep and sinusoidal oscillation.

Creep: Let us start with the creep experiment. Assume that for t<0t<0, the sample is at mechanical equilibrium and no load is applied, σ=0\psigma = 0. At t=0t=0, a stress jump of Δσ>0\Delta \psigma >0 is applied, and that value of stress is maintained for t>0t>0. How does the material respond? Definitely, at t<0t<0, there is vanishing strain, γ=0\gstrn = 0. To understand what happens at t=0t=0, we consider the Maxwell model (5.12), and integrate that differential equation over a small time-interval of duration δ\delta that includes the instant t=0t=0. This integration lads to:

∫−δ/2δ/2σ˙ dt=Δσ=∫−δ/2δ/2G γ˙ dt=GΔγ ,\int^{\delta/2}_{-\delta/2} \dot{\psigma} \ dt= \Delta \psigma = \int^{\delta/2}_{-\delta/2} G \ \dot{\gstrn} \ dt = G \Delta \gstrn \ ,

where we have neglected a contribution of the order δ\delta from the second term on the right hand side of (5.12). This means, that the imposed stress jump results in an immediate strain jump of magnitude Δγ=Δσ/G\Delta \gstrn = \Delta \psigma / G. And what happens at t>0t>0? To that end, we again consider the Maxwell model (5.12). Since the stress is held constant for t>0t>0, one may neglect the left hand side in (5.12), and one finds the simple relation (with constant value for the stress):

γ˙=η−1Δσ .\dot{\gstrn} = \eta^{-1} \Delta \psigma \ .

In other words, the strain γ\gstrn increases linearly in time, at a constant rate given by Δσ/η\Delta \psigma / \eta.

Sinusoidal oscillation: In this case, a time-dependent strain is imposed of the form

γ(t)=γ0 sin⁡(ω t) ,\gstrn(t) = \gstrn_0 \ \sin(\omega \ t) \ ,

where ω\omega denotes the angular frequency. To study the mechanical response of the Maxwell element under this deformation, we start with writing the Boltzmann integral (5.14) in a slightly modified form (transformation of variables from t′t' to s=t−t′s = t-t'),

σ(t)=∫0∞G(s) γ˙(t−s) ds .\psigma(t) = \int^{\infty}_0 G(s) \ \dot{\gstrn}(t-s) \ ds \ .

Using this relation, together with the oscillatory strain (5.18), and employing the general relation cos⁡(a−b)=cos⁡(a)cos⁡(b)+sin⁡(a)sin⁡(b)\cos(a-b) = \cos(a)\cos(b)+\sin(a)\sin(b), one obtains

σ(t)=γ0 G′(ω) sin⁡(ω t)+γ0 G′′(ω) cos⁡(ω t) ,\psigma(t) = \gstrn_0 \ G'(\omega) \ \sin(\omega \ t) + \gstrn_0 \ G''(\omega) \ \cos(\omega \ t) \ ,

where we have defined the so-called storage modulus G′G' and loss modulus G′′G'' by

G′(ω)=ω∫0∞G(s) sin⁡(ω s) ds ,G'(\omega) = \omega \int^{\infty}_0 G(s) \ \sin(\omega \ s) \ ds \ ,
G′′(ω)=ω∫0∞G(s) cos⁡(ω s) ds .G''(\omega) = \omega \int^{\infty}_0 G(s) \ \cos(\omega \ s) \ ds \ .

These are the Fourier-transforms of the relaxation modulus G(s)G(s).

According to (5.20), the storage modulus G′(ω)G'(\omega) determines the magnitude of the stress response that is in-phase with the applied deformation (5.18) (proportional to sin⁡(ω t)\sin(\omega \ t)), and thus describes the elastic-like behavior. In contrast, the loss modulus G′′(ω)G''(\omega) determines the magnitude of the stress response that is out-of-phase with the applied deformation (5.18), but in-phase with the applied rate (proportional to cos⁡(ω t)\cos(\omega \ t)), and thus describes the viscous-like behavior; this explains why G′′G'' is called the “loss” modulus.

There are then two ways to quantify the material behavior. Either, by knowledge of the entire relaxation modulus as a function of time, G(t−t′)G(t-t'), or my measuring in oscillatory measurements the two moduli G′(ω)G'(\omega) and G′′(ω)G''(\omega). However, it must be pointed out that the G′(ω)G'(\omega) and G′′(ω)G''(\omega) must be known not only at one specific frequency, but rather (ideally) at all frequencies, or at least in a wide frequency range.

In order to make the notion of in-phase and out-of-phase with the applied deformation more clear, the relation (5.20) is often rewritten in the form[2]

σ(t)=γ0 ∣G⋆(ω)∣ sin⁡(ωt+δ(ω)) ,\psigma(t) = \gstrn_0 \ |G^\star(\omega)| \ \sin(\omega t + \delta(\omega)) \ ,

with the definitions

∣G⋆(ω)∣=G′2(ω)+G′′2(ω) ,|G^\star(\omega)| = \sqrt{G'^2(\omega)+G''^2(\omega)} \ ,
tan⁡δ(ω)=G′′(ω)G′(ω) ,\tan \delta(\omega) = \frac{G''(\omega)}{G'(\omega)} \ ,

where the quantity δ(ω)\delta(\omega) is called the phase shift, i.e. the lag of the stress response with respect to the applied deformation (5.18) (see Figure 5.5). It is thus the ratio of loss to storage modulus that determines how much the stress response is in-phase with the applied deformation.

Illustration of the phase shift \delta between the imposed strain \gstrn and the stress response \psigma.

Figure 5.5:Illustration of the phase shift δ\delta between the imposed strain γ\gstrn and the stress response σ\psigma.

While the relations (5.21) and (5.22) are the general expressions in terms of the relaxation modulus G(s)G(s), it can be shown with the aid of the special relaxation modulus (5.15), that the storage and loss moduli for the Maxwell element are given by the relations (see Figure 5.6)

G′(ω)=G (ωτ)21+(ωτ)2 ,G'(\omega) = G \ \frac{(\omega \tau)^2}{1 + (\omega \tau)^2} \ ,
G′′(ω)=G ωτ1+(ωτ)2 .G''(\omega) = G \ \frac{\omega \tau}{1 + (\omega \tau)^2} \ .

Consequently, the phase shift of the Maxwell element becomes

tan⁡δ(ω)=1ωτ .\tan \delta(\omega) = \frac{1}{\omega \tau} \ .

It is rather illuminating to study for (5.28) the limiting cases of very fast or very slow deformation, and check whether they agree with the intuitive discussion presented in Section 5.3. This is left as an exercise for the reader.

Storage modulus G' and loss modulus G'' for the Maxwell element.

Figure 5.6:Storage modulus G′G' and loss modulus G′′G'' for the Maxwell element.

The notion of G′′(ω)G''(\omega) as a quantity related with “loss” (in other words: dissipation) can also be seen by the following argument. Using the relation (5.3) for the work done on the system, and applying that to a system described by the constitutive relation (5.20) with applied deformation (5.18), one obtains for the work done in one full cycle

ΔWcycle=∫02π/ωσ γ˙ dt=γ02 ω∫02π/ω(G′(ω) sin⁡(ωt)+G′′(ω) cos⁡(ωt)) cos⁡(ωt) dt=γ02 ω G′′(ω)∫02π/ωcos⁡2(ωt) dt=π γ02 G′′(ω) .\begin{aligned} \Delta W_{\rm cycle} &= \int^{2 \pi/\omega}_{0} \psigma \ \dot{\gstrn} \ dt \\ {} &= \gstrn^2_0 \ \omega \int^{2 \pi/\omega}_{0} \left( G'(\omega) \ \sin(\omega t) + G''(\omega) \ \cos(\omega t)\right) \ \cos(\omega t) \ dt \\ {} &= \gstrn^2_0 \ \omega \ G''(\omega) \int^{2 \pi/\omega}_{0} \cos^2(\omega t) \ dt \\ {} &= \pi \ \gstrn^2_0 \ G''(\omega) \ . \end{aligned}

Therefore, the work done in one full cycle depends only on G′′G'', but is independent of G′G'.

5.5Several Maxwell elements in parallel

The relaxation modulus (5.15) is an exponential decay with relaxation time τ\tau. Particularly, the Maxwell element describes a fluid, since for example after a step strain, the stress decays to zero after sufficiently long time. When studying common viscoelastic fluids, they also show that stress relaxation behavior, however, not with a single relaxation process, but with a superposition of relaxation processes, with respective time scales τi\tau_i. The observed behavior can be well described by a parallel arrangement of Maxwell elements, which are then called different Maxwell modes, and thus the relaxation modulus of such a viscoelastic fluid is not given by (5.15), but rather by its generalization

G(t−t′)=∑iGi(t−t′) ,G(t-t') = \sum_i G_i(t-t') \ ,

with the mode-specific relaxation modulus

Gi(t−t′)=Gi exp⁡(−t−t′τi) ,G_i(t-t') = G_i \ \exp\left(-\frac{t-t'}{\tau_i}\right) \ ,

with τi\tau_i the relaxation time of mode ii. Of course, the presence of different modes has ramifications for the loss and storage moduli, G′G' (5.21) and G′′G'' (5.22). In the multimode case, they are not anymore given by (5.26) and (5.27), but rather by their multimode counterparts

G′(ω)=∑iGi (ωτi)21+(ωτi)2 ,G'(\omega) = \sum_i G_i \ \frac{(\omega \tau_i)^2}{1 + (\omega \tau_i)^2} \ ,
G′′(ω)=∑iGi ωτi1+(ωτi)2 .G''(\omega) = \sum_i G_i \ \frac{\omega \tau_i}{1 + (\omega \tau_i)^2} \ .

In order to identify the various parameters of the modes, sinusoidal oscillation measurements are preferred, for example over step-strain (meaning: stress relaxation). In stress relaxation, one should split up a decaying function into a superposition of various exponential decays. This is for practical purposes cumbersome. Much easier and more accessible are sinusoidal oscillation measurements: The storage modulus G′(ω)G'(\omega) transitions from one plateau value to another at the characteristic frequencies ω=τi−1\omega = \tau^{-1}_i, and even more prominent are the peaks of the loss modulus G′′(ω)G''(\omega) at the same characteristic frequencies ω=τi−1\omega = \tau^{-1}_i (see Figure 5.7). It is significantly easier to discriminate superposed peaks in G′′(ω)G''(\omega), rather than to discriminate superposed exponential decays in G(t−t′)G(t-t'). This is the reason why usually oscillatory measurements are used to characterize a viscoelastic fluid.

Illustration of the loss modulus G'' for a two-mode Maxwell model with relaxation times \tau_1 and \tau_2.

Figure 5.7:Illustration of the loss modulus G′′G'' for a two-mode Maxwell model with relaxation times τ1\tau_1 and τ2\tau_2.

5.6Kelvin-Voigt element

As an alternative to the Maxwell element, in the literature also the so-called Kelvin-Voigt element is used. It consists from the same elements as he Maxwell element, a Hookean and a Newtonian element, however, in the Kelvin-Voigt element these elements are arranged in parallel (see Figure 5.8). The Kelvin-Voigt element has a rather undesirable feature for most practical mechanical engineering purposes. Namely, in fast loading (high rate such as in shock; step-strain experiment), the Newton element gets completely stiff, meaning that the Kelvin-Voigt element is not deformed at all. For this reason, we do not discuss the Kelvin-Voigt element any further in this lecture.

Kelvin-Voigt element: Parallel coupling of a spring and a dashpot.

Figure 5.8:Kelvin-Voigt element: Parallel coupling of a spring and a dashpot.

5.7Standard Solid element

For modeling purposes, or for the stability of numerical implementations, the Maxwell element is extended to include a Hookean element in parallel to the Maxwell element (see Figure 5.9). While within the Maxwell element the strain rates are to be added (see (5.10)), the parallel coupling of the Maxwell element with the additional Hookean element requires adding the corresponding stresses. This new composed element is called Standard Solid element, or Standard Solid model.

Standard Solid element.

Figure 5.9:Standard Solid element.

Most common is the case, where the elastic modulus G1G_1 in the Maxwell element is much larger than the elastic modulus G2G_2 of the additional Hookean element, G1≫G2G_1 \gg G_2. In this case, the mechanical response in the high-deformation rate regime is dominated by the Maxwell element (since the Newtonian element is rather stiff and thus the load is effectively carried by the G1G_1-spring. However, at very low deformation rates, only rather small loads are built up over the Maxwell element (Newtonian element basically flows), and so the additional parallel G2G_2-elastic element carries the load.

Rather than going into more details here, we leave this to the interested reader. For example, one could examine the behavior of the Standard Solid element in the four standard deformation protocols.

For completeness, it is mentioned that if a spring is combined in parallel not only with a single Maxwell element (as in Figure 5.9), but rather with several Maxwell elements in parallel, then this model is called the Generalized Maxwell element, or Generalized Maxwell model.

5.8Check your understanding

Footnotes
  1. Carefully write down σ(t+Δt)−σ(t)\psigma(t+\Delta t) - \psigma(t), and then look at the limit of (σ(t+Δt)−σ(t))/Δt(\psigma(t+\Delta t) - \psigma(t))/\Delta t when Δt→0\Delta t \to 0.

  2. The equivalence of the relation (5.23) with (5.20) can be shown by using standard trigonometric relations.