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6 Viscoplasticity

In this Chapter, we extend our considerations of the Maxwell element in the previous Chapter. Particularly, the purpose of this Chapter is to discuss the following issues:

In other words, we have discussed in the previous Chapter linear viscoelasticity. In this Chapter, we seek nonlinear modifications of that approach, particularly as far as stress- and temperature-dependencies are concerned.

Looking at the Maxwell element discussed in the previous Chapter, there are in principle two spots where a stress-dependence could be introduced: First, the Hookean element could be made nonlinear, meaning that the modulus GG becomes stress-dependent. In this Chapter we concentrate instead on the second possibility, which is to make the viscosity stress-dependent. It will be discussed that this does not only lead to quantitative changes in the material behavior, rather it amounts to qualitatively different mechanical response. By explaining the physical origins of this stress-dependence of the viscosity, it also becomes clear that the mechanical response of a viscoelastic material must depend substantially on temperature, the second main topic in this Chapter.

6.1Kinetics of structural rearrangements

In Section 5.3, “Origin of viscoelasticity, time scales”, we have discussed the relevance of structural rearrangements on the microscopic scale to relax stresses that arise due to macroscopically imposed deformation. The conclusion was that viscous-like behavior on the macroscopic scale has its origin in small-scale kinetics of the constituent particles (atoms, molecules, ...).

We now look in more detail into this small-scale kinetics. A wide-spread working hypothesis all across natural sciences and engineering disciplines is that (rate-limiting, barrier-crossing) kinetics can be described by an Arrhenius law,

k=k0 exp⁡(−UkBT) ,k = k_0 \ \exp\left(-\frac{U}{\kB T}\right) \ ,

with kk the kinetic rate, k0k_0 the kinetic-rate prefactor, UU the energy barrier, kB\kB the Boltzmann constant, and TT the absolute temperature. In this concept, one is obviously not interested in the fast vibrations of atoms and the like, rather one looks for transitions that lead to significant changes in the structure, something that we as mechanics people would identify with an inelastic/plastic event.

The above relation shows that such structural rearrangements depend on the ratio of the energy barrier UU to the thermal energy kBT\kB T. This implies that the kinetics can be accelerated (slowed down) upon increasing (decreasing) the temperature. However, there is also other means to accelerate the kinetics of structural transitions. Eyring (Krausz, A., Eyring, H., 1975. “Deformation Kinetics”. Wiley-Interscience, London) has put forward the following idea of stress-assisted kinetics:

Modification of the energy barriers due to the applied load.

Figure 6.1:Modification of the energy barriers due to the applied load.

Imagine that the microstructure can change in two possible “directions”. Then, in equilibrium, the rates to transition in either of the two directions, denoted by k>k_> and k<k_<, are equal, namely they are both given by (6.1). However, when a load is applied in the form of a stress, there is a bias to transition preferentially in one of the two directions. In terms of the Arrhenius relation (6.1) this effect can be captured by noting that the (free) energy barrier is modified by the applied stress. More specifically, Eyring stated that the energy barrier is modified in a linear manner in terms of stress,

U>=U−v σ ,U<=U+v σ ,\begin{aligned} U_> &= U - v \ \psigma \ , \\ U_< &= U + v \ \psigma \ , \end{aligned}

which implies that the energy barrier in the “forward” direction is decreased, while the energy barrier in the “backward” direction is increased (see Figure 6.1). The material parameter vv (units: [m3^3]), v>0v > 0, is introduced for dimensional reasons, and is called the activation volume. This leads to an imbalance in forward and backward rates that reads as follows:

k>−k<=k0 [exp⁡(−U>kBT)−exp⁡(−U<kBT)]=k0 exp⁡(−UkBT) [exp⁡(v σkBT)−exp⁡(−v σkBT)]=2 k0 exp⁡(−UkBT) sinh⁡(v σkBT) .\begin{aligned} k_> - k_< &= k_0 \ \left[\exp\left(-\frac{U_>}{\kB T}\right) - \exp\left(-\frac{U_<}{\kB T}\right)\right] \\ {}&= k_0 \ \exp\left(-\frac{U}{\kB T}\right) \ \left[\exp\left(\frac{v \ \psigma}{\kB T}\right) - \exp\left(-\frac{v \ \psigma}{\kB T}\right)\right] \\ {}&= 2 \ k_0 \ \exp\left(-\frac{U}{\kB T}\right) \ \sinh\left(\frac{v \, \psigma}{\kB T}\right) \ . \end{aligned}

If one then identifies the imbalance in rates, k>−k<k_> - k_<, with the macroscopically observed plastic (=unrecoverable) strain rate γ˙p\psr, then one can write, as far as the stress-dependence is concerned,

γ˙p∝sinh⁡(v σkBT) .\psr \propto \sinh\left(\frac{v \, \psigma}{\kB T}\right) \ .

That plastic strain rate in turn can be used to define the viscosity in the following way:

η(σ)=σγ˙p(σ)=η0 v σkBTsinh⁡(v σkBT) ,\begin{aligned} \eta(\psigma) &= \frac{\psigma}{\psr(\psigma)} \\ {}&= \eta_0 \ \frac{\frac{v \, \psigma}{\kB T}}{\sinh\left(\frac{v \, \psigma}{\kB T}\right)} \ , \end{aligned}

where the prefactor η0\eta_0 has been introduced for convenience. Particularly, one finds (since sinh⁡(x)≃x\sinh(x) \simeq x for x≪1x \ll 1) that η(σ)≃η0\eta(\psigma) \simeq \eta_0 for vanishingly small loads, v σ≪kBTv \, \psigma \ll \kB T. On the other hand, the viscosity η(σ)\eta(\psigma) drops rapidly below η0\eta_0 for large loads, v σ≫kBTv \, \psigma \gg \kB T (see Figure 6.2). The viscosity function defined in (6.5) is called the Eyring viscosity.

Hyperbolic sine function, and illustration of the nonlinearity in the Eyring viscosity.

Figure 6.2:Hyperbolic sine function, and illustration of the nonlinearity in the Eyring viscosity.

The Eyring viscosity (6.5) is particularly useful to describe solid polymers, and it has an intuitive origin. On the other hand, for example in metals, other relations are used (see also lecture slides). Most common in the field of metal plasticity is to work with a plastic strain rate that depends through a power-law on the applied stress, γ˙p∝σm\psr \propto \psigma^m. The viscosity is then defined correspondingly as η=σ/γ˙p∝σ1−m\eta = \psigma/\psr \propto \psigma^{1-m}. Usually, one has for the power-law exponent m≫1m \gg 1, leading, as in the Eyring case, to a rather strong nonlinearity. In the case of metal plasticity, the stress-dependence of the viscosity originates from the collective effects in the dynamics of dislocations, the carriers of plastic deformation in crystals.

6.2Viscoplastic model

In the previous section, possible origins for the stress-dependence of the viscosity have been discussed. Using the Maxwell model (5.12) discussed in the case of linear viscoelasticity, taking the stress-dependence into account leads to

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

with the now stress-dependent characteristic time scale

τ(σ)=η(σ)G .\tau(\psigma) = \frac{\eta(\psigma)}{G} \ .

One viewpoint of (6.6) is to assume that the relation η=η(σ)\eta=\eta(\psigma) is given. On the other hand, one can also take the viewpoint that the material at hand be described by a viscoplastic model of the form (6.6), and the question is then how the relation η=η(σ)\eta=\eta(\psigma) can be determined from experiments. Of course, the standard experiments come to mind: step-strain, step-strain rate, (sinusoidal) oscillation, and creep. For step-strain and creep, the reader may follow procedures similar as in Linear Viscoelasticity. As far as sinusoidal oscillation is concerned, we recall from Linear Viscoelasticity that the analysis there profited essentially from the fact that the model was linear[1]. One can already anticipate that the nonlinearity in (6.6) due to the stress dependence of the relaxation time will complicate the analysis of oscillatory response significantly. Therefore, we concentrate here on the case of a step-strain rate experiment.

In the step-strain rate experiment, let us consider only the situation in which the stress σ\psigma has come to a stationary state, σsteady\psigma_{\rm steady}. According to (6.6) we have have the following condition:

γ˙=σsteadyη(σsteady) .\dot{\gstrn} = \frac{\psigma_{\rm steady}}{\eta(\psigma_{\rm steady})} \ .

This equation can be used to examine the the dependence of the steady “yield” stress σsteady\psigma_{\rm steady} as a function of the applied (constant) strain rate γ˙\dot{\gstrn}. Obviously, the found relation depends on the viscosity function η(σ)\eta(\psigma). In turn, this implies that measuring the relation σsteady=σsteady(γ˙)\psigma_{\rm steady} = \psigma_{\rm steady}(\dot{\gstrn}) allows to access the relation η(σ)\eta(\psigma). For example, for the case of the Eyring viscosity (6.5), the steady-state condition (6.8) assumes the form

γ˙=kBT/vη0sinh⁡(v σsteadykBT) .\dot{\gstrn} = \frac{\kB T/v}{\eta_0} \sinh\left(\frac{v \ \psigma_{\rm steady}}{\kB T}\right) \ .

Using v σsteady≫kBTv \ \psigma_{\rm steady} \gg \kB T (which can be justified a posteriori by analyzing experimental data), one can use the approximation sinh⁡(x)≃exp⁡(x)/2\sinh(x) \simeq \exp(x)/2, which leads to

γ˙=kBT/v2η0exp⁡(v σsteadykBT) .\dot{\gstrn} = \frac{\kB T/v}{2 \eta_0} \exp\left(\frac{v \, \psigma_{\rm steady}}{\kB T}\right) \ .

The last relation can be inverted readily to find the dependence of the steady-state yield stress σsteady\psigma_{\rm steady} on the applied constant strain rate γ˙\dot{\gstrn},

σsteady(γ˙)=kBTvln⁡(2η0γ˙kBT/v)=kBTv[ln⁡γ˙+ln⁡(2η0kBT/v)] .\psigma_{\rm steady}(\dot{\gstrn}) = \frac{\kB T}{v} \ln\left(\frac{2 \eta_0 \dot{\gstrn}}{\kB T/v}\right) = \frac{\kB T}{v} \left[ \ln\dot{\gstrn} + \ln\left(\frac{2 \eta_0}{\kB T/v}\right) \right] \ .

In particular, we find the following relation that allows the experimental measurement of the activation volume,

d σsteady(γ˙)d ln⁡γ˙=kBTv .\frac{d \, \psigma_{\rm steady}(\dot{\gstrn})}{d \, \ln\dot{\gstrn}} = \frac{\kB T}{v} \ .

In other words, when plotting the steady-state yield stress as a function of the natural logarithm of the applied strain rate, the slope in that curve is directly related to the activation volume. And, indeed, this is how in practice the activation volume for a material is determined experimentally (see Figure 6.3).

Dependence of the stress-strain behavior of glassy polycarbonate on the applied rate of deformation. The dots indicate the yield stress, for each rate of deformation.

Figure 6.3:Dependence of the stress-strain behavior of glassy polycarbonate on the applied rate of deformation. The dots indicate the yield stress, for each rate of deformation.

6.3Terminology

In this section, we differentiate between different forms of non-elastic behavior, and clarify particularly the difference between three terms, namely: viscoelasticity, elasto-plasticity, and elasto-viscoplasticity.

6.4Effect of temperature: Time-temperature superposition principle

At finite absolute temperature, there is always some degree of mobility in the system. For example, one can show that for a material at finite temperature TT, the average kinetic energy of a particle (atom) is proportional to TT. As a consequence, there is increased (molecular) mobility in the system as the temperature TT is increased. As an illustration, one can consider the melting of ice:

Melting dynamics of ice (Masakazu Matsumoto)

Molecular dynamics simulation of ice crystal melting (shityakoff)

What does the increased temperature mean for macroscopically measurable quantities that relate to the dynamics? Well: as the temperature is increased, and as the particles move more rapidly, the time scale for structural rearrangements decreases, as does the viscosity of the system (see (5.13) for the relation between the time scale τ\tau and the viscosity η\eta).

Dependence of the mechanical response on the frequency of the applied deformation and on temperature.

Figure 6.4:Dependence of the mechanical response on the frequency of the applied deformation and on temperature.

An illustrative example is a dense system of polymer chains that are entangled (like a pot of intertwined spaghetti). In this system, the time for disentanglement is the longest time scale in the system. Let us first study the material behavior of this system at a fixed temperature, with increasing frequency (see Figure 6.4). If the frequency is very high, and the rate of deformation thus very fast, the entangled chains do not have the time to disentangle in order to relax the rapidly building-up stress, and the system therefore reacts as if the entanglements were permanently fixed (chemically cross-linked). Decreasing the frequency to very small values leads to a deformation rate that is so small that the chains do have the time to rearrange the entanglement-structure to relax the stresses, and therefore the system behaves fluid-like. While this is an argumentation along the lines of changing frequency at a fixed temperature, one can also look at the change in material response at a fixed frequency while changing the temperature TT. In analogy to the arguments just mentioned, one can anticipate the following scenario: At a fixed frequency and very low temperature, the mobility in the system is rather small with a characteristic rate of rearrangement much smaller than the applied frequency, and thus the material behaves as a chemically cross-linked system. If, however, the temperature is increased drastically, the mobility is so much increased that even entanglement-rearrangements are involved in relaxing the imposed deformation. In short, increasing the temperature (at fixed frequency) shows the same effect as decreasing the frequency (at fixed temperature). The questions is now: How can we rationalize that finding, and make use of it in viscoelastic and elasto-viscoplastic models?

To study the effect of temperature on the rate-dependent behavior of materials, it is useful to define the time-temperature shift factor for a certain relaxation process jj,

aT0,j(T)=τj(T)τj(T0)(in general) .a_{T_0,j}(T) = \frac{\tau_j(T)}{\tau_j(T_0)} \qquad \textrm{(in general)} \ .

If the material behavior is known at a certain temperature T0T_0, and a corresponding model has been set up, then one can also apply that model to the behavior at another temperature TT, by replacing all time scales τj(T0)\tau_j(T_0) in the model by τj(T)\tau_j(T). Notably, one needs to make that replacement for all processes jj. This implies that one in principle would need to know the time-temperature shift factors aT0,j(T)a_{T_0,j}(T) for all processes. This is in general a formidable task, meaning that the experimental determination of the different shift factors is difficult. However, it turns out that for many polymeric materials the time-temperature shift factor is the same for all (measurable) processes (meaning: the time-temperature shift factor is independent of jj),

aT0(T)=τj(T)τj(T0)(special case) ,a_{T_0}(T) = \frac{\tau_j(T)}{\tau_j(T_0)} \qquad \textrm{(special case)} \ ,

in which case the material is called to be thermorheologically simple. The (experimentally supported) assumption that the effect of temperature can be included in a material description by an appropriate rescaling of the time-scale is called the time-temperature superposition principle. An example for the time-temperature shift factor is shown in Figure 6.5.

Example for the time-temperature shift factor, above the glass transition temperature T_{\rm g}.

Figure 6.5:Example for the time-temperature shift factor, above the glass transition temperature TgT_{\rm g}.

We leave it as an exercise for the reader to examine the effect of lowering the temperature on the behavior of a Maxwell element in the four standard measurements (step-strain, step-strain rate, (sinusoidal) oscillation, and creep).

The time-temperature superposition principle of thermorheologically simple materials is very beneficial for practical measurements. Imagine, for example, that you want to measure in a step-strain experiment the relaxation modulus G(t,T0)G(t, T_0), at a certain temperature T0T_0. Most probably, the experimental set-up you are using has a limited time-resolution: On the one hand, there is a lower bound on the resolvable dynamics tmint_{\rm min}, in the sense that the mechanics of the apparatus has certain inertia, and thus very small time-scales and fast deformations are inaccessible. On the other hand, there is an upper bound on the resolvable dynamics, tmaxt_{\rm max}, for example because you can not keep the temperature constant at T0T_0 over a long enough period. In other words, you can only measure the relaxation modulus G(t,T0)G(t,T_0) for times tmin<t<tmaxt_{\rm min} < t < t_{\rm max}. For thermorheologically simple materials, one can still determine the relaxation modulus G(t,T0)G(t, T_0) for times tt outside the range tmin<t<tmaxt_{\rm min} < t < t_{\rm max}, as described in the following.

Imagine that the relaxation modulus G(t,T0)G(t, T_0) is given by the relation (5.15), where for simplicity we restrict our attention to a single mode only. In this expression, one observes that the relaxation modulus is a function of the ratio t/τt/\tau with τ\tau the relaxation time, and no other time-dependence occurs. Particularly, one can write the relaxation modulus in the form

G(t,T0)=f(tτ(T0)) ,G(t, T_0) = f\left(\frac{t}{\tau(T_0)}\right) \ ,

for a certain function ff. Using the time-temperature shift factor (6.13), one can rewrite this expression into

G(t,T0)=f(tτ(T0))=f(t aT0(T)τ(T))=G(t aT0(T),T) .G(t, T_0) = f\left(\frac{t}{\tau(T_0)}\right) = f\left(\frac{t \ a_{T_0}(T)}{\tau(T)}\right) = G(t \ a_{T_0}(T), T) \ .

In other words, the value of the relaxation modulus at a certain time tt measured at temperature T0T_0 is equal to the relaxation modulus at time t aT0(T)t \ a_{T_0}(T) measured at temperature TT. What does that mean in practice? Suppose that you want to determine the relaxation modulus at a very short time t<tmint < t_{\rm min} (which is outside the experimentally accessible window) at temperature T0T_0. So, you are interested in fast processes. These fast processes are slowed down upon decreasing the temperature to TT (therefore: T<T0T < T_0), which is described by (6.13) with aT0(T)>1a_{T_0}(T) > 1 for T<T0T < T_0. The relation (6.16) then tells you that, instead of measuring the relaxation modulus at time tt and temperature T0T_0, you can rather measure the relaxation modulus at a lower temperature T<T0T < T_0 but at a longer time t aT0(T)t \ a_{T_0}(T) (note that t aT0(T)>tt \ a_{T_0}(T) > t). The idea is thus to go to so low temperature TT that this “longer time” falls within the possible measurement window, t aT0(T)>tmint \ a_{T_0}(T) > t_{\rm min}. After performing this measurement at TT, one can “shift” the result according to (6.16), in order to obtain eventually the time-dependence of G(t,T0)G(t, T_0) over a time-range much wider than tmin<t<tmaxt_{\rm min} < t < t_{\rm max}. This procedure is demonstrated in Figure 6.6.

Using the time-temperature superposition principle for effectively measuring the relaxation modulus over more than 15 decades (!) in time.

Figure 6.6:Using the time-temperature superposition principle for effectively measuring the relaxation modulus over more than 15 decades (!) in time.

While the above procedure (changing temperature- and time-window) was explained on the example of a single-mode model, the question arises how to do that for a Maxwell model with multiple modes, in other words with multiple relaxation times. This is exactly the point when it is useful to know whether a material is thermorheologically simple. For this latter class of materials, one can use the same shift factor for all processes. As a consequence, the relation outlined in (6.16) can be used in exactly the same way also for multimode materials, for example as described by (5.30) and (5.31) .

Footnotes
  1. In other words, an imposed strain with angular frequency ω\omega resulted in a, albeit phase-shifted, response that oscillates with the same frequency ω\omega, and no higher harmonics (meaning, no oscillations with frequencies 2ω2 \omega, 3ω3 \omega, ...) occurred.