While viscoelastic, adhesive contact rupture of simple indenters is well studied, contact formation has received much less attention. Here, we present simulations of the formation of contact between various power law indenters and an adhesive, viscoelastic foundation. For all investigated indenters, we find that the macroscopic relaxation time τ scales approximately with 1/ρ1.8, where ρ is the range of adhesion. The prolongation of contact formation with Tabor parameter is rationalized by the increased dissipation that short-range adhesion causes on a moving crack.

The modeling of mechanical contacts between elastomers and rigid counterfaces has advanced substantially in the recent past.1–3 In particular, the comparison between simulated contact configurations and real-laboratory images has reached new levels, mainly thanks to improved capabilities of computing and measuring detailed features in partial contacts of nominally flat surfaces.1,4–8 However, the progress made pertains mostly to situations where either the experiment is conducted quasi-statically or multi-scale roughness is insignificant. Viscoelastic simulations with roughness on separate length scales remain scarce.8–10 As a consequence, it remains difficult to ascertain or to predict when contact hysteresis in a given system is mostly viscoelastic in nature11 or caused by elastic multistability12–14 and whether their effects are deemed additive10 or inseparable.8 When assessing contact hysteresis, it is as important to describe contact formation as contact rupture.15 However, despite continuous progress in the simulation of viscoelastic, adhesive contacts,16–20 contact formation is explored rather little although it is similarly important as contact rupture. It could be one reason for the so-called Monday morning problem, which refers to the sticking of valves in production engines after resting over the weekend. Further applications, where (slow) contact formation matters, are hydraulic and pneumatic seals or adhesive gripping devices.

The difficulty of simulating adhesion-driven contact formation involving soft matter is that the short-range nature of adhesion must be accounted for, even for macroscopic objects. First, noncontact puts much greater demands on the range of adhesion than contact:15,21 While a Tabor parameter μT ≈ 5 (μT is a dimensionless measure inversely proportional to the range of adhesion and introduced in detail further below) suffices to reproduce the μT load–displacement curves under retraction, the energy loss would be less than 50% of the real value, due to a premature jump into contact. Unfortunately, short-range adhesion requires a modeler to use small mesh sizes to avoid discretization artifacts, most notably lattice trapping.15 Making matters worse, the errors in energy hysteresis disappear only with the inverse cube of the linear mesh-element size.15 Second, short-range adhesion enhances the dissipation of a moving crack or contact line,22–26 whereby not only crack opening but also crack closure is impeded, which in turn puts large demands on the computing time.

The discussion above implies that simulating effectively viscoelastic processes using relatively coarse scales might be achievable by reinterpreting the time scales used in the viscoelastic model.This would be possible if multiplying the range of adhesion by a factor s accelerated the dynamics by a power of s. Testing for the possibility of such a mapping was the original motivation for the research reported in this work. However, the simulations can also serve as a test for theoretical predictions on contact closure and extend the number of geometries, for which gap closure is investigated. In this context, our focus is on indenter shapes, where the height of the indenter is a power law of the distance from the indenter’s symmetry axis. This problem class offers the greatest potential for us to exploit the similarity of solutions.

The remainder of this work is organized as follows: The methods used are laid out in Sec. II, results are presented in Sec. III, and conclusions are drawn in Sec. IV. Some scaling arguments allowing the Tabor parameter to be generalized to adhesive power law indenters are given in the  Appendix.

We use Green’s function molecular dynamics (GFMD),27 which is a boundary-element method for the simulation of linearly (visco)elastic contact problems assuming elastic bodies to be isotropic in planes normal to their (originally flat) surface and to be periodically repeated in that plane. We focus on normal, frictionless contacts within linear elasticity. Our systems consist of various perfectly rigid indenters and a homogeneous and isotropic, linearly viscoelastic body described in the continuum limit.

The shape of the indenter is given by
(1)
where R has the unit of length and corresponds to a radius of curvature for a Hertzian (n = 2) indenter, while r is the distance from the indenter’s symmetry axis. For a conical indenter (n = 1), h(r) could be written as h(r) = r tan φ, in order to implement different opening angles φ. Investigated exponents are n = 1 for a conical indenter, n = 2 for a Hertzian indenter, and n = 3 as well as n = 4 as crude approximations for a flat punch. A true flat punch has no interesting contact formation dynamics, as its instantaneous contact radius is identical to the relaxed one.
Indenter and elastic body interact through a cohesive-zone model that is twice differentiable everywhere but in one isolated point, which proves to be useful for numerical or stability reasons.15 It is given by an interaction potential density of
(2)
Here, g refers to the gap or interfacial displacement between elastomer and indenter, γ is the energy gained per unit area when indenter and elastomer touch, while ρ is the range of adhesion. In all investigated systems, a numerical value of γ = 0.01 E*R is assigned. The numerical value of ρ was adjusted according to the individual Tabor parameters. In principle, ρ could be set to a smaller value for negative than for positive gaps to better mimic hard-wall repulsion. However, since all reported simulations addressed rather short-ranged adhesion and thus small ρ, we used the same value for ρ for attraction and repulsion.
The elastic energy of a relaxed body (under an external surface stress) is given by
(3)
where q is an in-plane wave vector, or wave number for one-dimensional interfaces, q is its magnitude, while E* is the static contact modulus and ũ(q) the Fourier transform of the displacement field. However, as we study a viscoelastic system, E* is made frequency dependent. Our default model consists of a single Maxwell element in parallel with a spring, yielding a frequency-dependent contact modulus of
(4)
with sE*/E0*=100, where E0* and E* are the quasi-static and the high-frequency elastic moduli, respectively. The model is implemented as described in Ref. 8. E0* is used as the unit for pressure, while times are reported in units of τMxw, unless stated otherwise. Any deviation from our default model is explicitly pointed out. For example, in one case, the surface modes are coupled to three rather than to one Maxwell element. The real and imaginary parts of E*(ω) are shown in Fig. 1 for the three-element model and the default, one-element model. The “weights” E0(n) and relaxation times τMxw(n) in the three-element models are chosen as E0n+1=6E0n and τMxw(n+1)=τMxw(n)/6.
FIG. 1.

Absolute value |E*′(ω)| (top), real part E*′(ω) (middle), and imaginary part E*″(ω) (bottom) of the contact modulus for a one-element (1-el, solid lines), standard linear-solid model and a three-element (3-el, dashed and dotted lines) model. The frequency is expressed in inverse units of τMxw of the one-element model (blue line), while the data for the three-element are shifted one time to have a similar high-frequency (dashed, blue line) and one time to have a similar low-frequency (dotted, orange line) modulus as the one-element model.

FIG. 1.

Absolute value |E*′(ω)| (top), real part E*′(ω) (middle), and imaginary part E*″(ω) (bottom) of the contact modulus for a one-element (1-el, solid lines), standard linear-solid model and a three-element (3-el, dashed and dotted lines) model. The frequency is expressed in inverse units of τMxw of the one-element model (blue line), while the data for the three-element are shifted one time to have a similar high-frequency (dashed, blue line) and one time to have a similar low-frequency (dotted, orange line) modulus as the one-element model.

Close modal

While a “brute-force” Fourier method is certainly not the most effective approach to address the questions in this paper, it is sufficiently efficient to obtain satisfying answers. Moreover, by addressing primarily line contacts having a formal interfacial dimension of D = 1, much of the computational overhead spent on not exploiting the symmetry of the problem in D = 2 is alleviated.

The most critical dimensionless parameter for a (force-free) adhesive contact of a Hertzian indenter is the Tabor parameter μT. It is inversely proportional to the range of adhesion and is designed such that μT ≫ 1 makes a (quasi-static) contact behave as in the limit for zero-range adhesion, which was first solved analytically by Johnson, Kendall, and Roberts (JKR)28 for n = 2 and D = 2. For arbitrary n at D = 2, the contact problem can be solved using Sneddon’s method.29,30 Less relevant for most real purposes, but easier to tackle numerically and theoretically, is long-range adhesion. For D = n, adhesion effectively acts like an external load that does not depend on ρ for ρ or μT → 0 when γ and R are fixed, as is readily seen using the Bradley model,31 which becomes exact in the long-range limit. Its analysis also reveals that a physically meaningful long-range-adhesion limit does not exist for nD, because the offset load vanishes (n > D) or diverges (n < D) for a diverging ρ at fixed γ and R.

Zheng and Yu32 generalized the Tabor parameter for arbitrary power law indenters to
(5)
after solving the contact mechanics of adhesive power law indenters in the Dugdale approximation. In the  Appendix, we identify the same expression using rather simple, dimensional analysis, which is also valid for an interfacial dimension of D = 1. In the following, we will usually report μT rather than the range of adhesion ρ. Note that the precise value for μT would differ if the ratio γ/σmax were used instead of ρ in Eq. (5).
In this work, we study exclusively crack closure dynamics under zero external load. We focus on the time evolution of the contact radius rc(t), which we define to be the distance from the indenter’s symmetry axis to the point where the tensile stress takes its maximum, specifically, the distance in a direction parallel to a main axis of the simulation cell rather than its diagonal, though the two measures are very close to each other and thus show identical scaling. A small relaxation run is done first, using “regular” rather than viscoelastic GFMD, during which the elastomer is allowed to relax to the shape that it would have under the assumption that E* rather than E0* was its static contact modulus. The estimates of quasi-static contact properties are obtained from similar calculations with the proper static contact modulus E0*. This way, initial contact radii rinrc(t = 0) and quasi-static contact radii rqsrc(t) can be determined with high accuracy. Results for rc(t) are reported in terms of a relaxation function defined as
(6)

While we do not yet have experimental reference data, it might be important to stress that it might be difficult to rigorously define rin in real experiments, since contact with a rigid counter body cannot be simply switched on as in a computer simulation, while inertial effects would prevent an immediate contact at t = 0+ with the high-frequency modulus from occurring. Thus, we expect deviations between our idealized model and real experiments in the very early stages of contact formation to be unavoidable.

While this study focuses on contact formation for different tip geometries, we first wish to analyze how details of the viscoelastic model affect the dynamics. To this end, Fig. 2 contrasts the gap closure for the one-element model and the three-element model introduced in Sec. II. Both rheological models reveal the same generic features of the crack closure process for power law indenters: Early-time dynamics, in the specific example for t ≲ 10 τMxw, a regime where the contact radius depends approximately logarithmically on time, i.e., for times 10 ≲ t/τMxw ≲ 104, and a final regime at t ≳ 104τMxw, which has an exponential time dependence according to
(7)
which defines the macroscopic or largest relaxation time τ. While the relaxation in the intermediate time curve is somewhat flattened for the three-element model compared to the one-element model, the contrast in different rc(t) curves in Fig. 2 appears somewhat less noticeable to the eye than those of the frequency-dependence of the elastic modulus shown in Fig. 1. Interestingly, though perhaps not surprisingly, the early-time (later-time) dynamics of the two models superimpose reasonably well when the relaxation times of the three-element model are scaled such that the high-frequency (low-frequency) E″(ω) or |E(ω)| exhibits similar behavior. In the following, we will merely consider the one-element model, widely known also as the standard linear solid (SLS).
FIG. 2.

Contact formation of the one-element model and the three-element model(s), whose frequency-dependent elastic modulus is shown in Fig. 1; D = 1, n = 2, μT = 7.2. Thin gray lines indicate the instantaneous contact radius for t → 0 as well as the final exponential approach (exp) to the quasi-static value rqs reached at t.

FIG. 2.

Contact formation of the one-element model and the three-element model(s), whose frequency-dependent elastic modulus is shown in Fig. 1; D = 1, n = 2, μT = 7.2. Thin gray lines indicate the instantaneous contact radius for t → 0 as well as the final exponential approach (exp) to the quasi-static value rqs reached at t.

Close modal

Similar crack closure dynamics as those just discussed are maintained when extending the range of Tabor parameters. To this end, C(t) rather than rc(t)/R is shown for different μT, one time for two-dimensional interfaces in Fig. 3 and one time, as before, for one-dimensional interfaces in Fig. 4. Similar behavior is revealed in both figures. A double logarithmic representation was chosen for them as to highlight differences in the functional form of C(t) during the early-time dynamics. Note that the time is expressed in units of τ, which allows us to reveal that C(t/τ) is quite insensitive to μT at sufficiently large t. The collapse of curves when represented as C(t/τ) improves with increasingly large μT. Factors and related information helpful to reconstruct the full rc(t/τ) are collected in Table I, however, each time only for the largest Tabor parameter.

FIG. 3.

Crack closure dynamics for different axisymmetric tips.

FIG. 3.

Crack closure dynamics for different axisymmetric tips.

Close modal
FIG. 4.

Crack closure dynamics for different one-dimensional tips.

FIG. 4.

Crack closure dynamics for different one-dimensional tips.

Close modal
TABLE I.

Quantities needed to reconstruct the full rc(t) dependence, for each investigated geometry at the largest investigated Tabor parameter μT. Radii are given in units of the (generalized) radius of curvature R and times in units of τMxw. τ1/2 is defined implicitly by C(τ1/2) = 1/2.

Dnrinrqsτ1/2τμTs
0.0021 0.062 130 1060 4.1 19 
0.11 0.46 23 910 41 5.9 
0.28 0.67 9.8 670 65 4.1 
0.41 0.78 6.6 750 79 3.5 
0.013 0.10 23 110 0.30 24 
0.17 0.52 3.7 83 3.0 7.2 
0.35 0.71 1.6 45 4.8 4.9 
0.48 0.81 1.0 36 5.8 4.2 
Dnrinrqsτ1/2τμTs
0.0021 0.062 130 1060 4.1 19 
0.11 0.46 23 910 41 5.9 
0.28 0.67 9.8 670 65 4.1 
0.41 0.78 6.6 750 79 3.5 
0.013 0.10 23 110 0.30 24 
0.17 0.52 3.7 83 3.0 7.2 
0.35 0.71 1.6 45 4.8 4.9 
0.48 0.81 1.0 36 5.8 4.2 

The increase in relaxation time compared to the times associated with the Maxwell element can certainly be related to the increased dissipation that short-range adhesion causes in a propagating crack.22,24,25 Initial dynamics are relatively fast, when the crack-tip radius is large and thus dissipation small10,26 but then slows down as the crack-tip radius becomes smaller, while the slopes of the displacement field increase. For the investigated tip shapes, we find the relaxation times to scale approximately with μT1.8. This is true for the ultimate relaxation time τ as well as intermediate relaxation times τx defined by C(τx) = x with x ≳ 0.5. To make the different data sets appear in a rather narrow range, the Tabor parameter was scaled (multiplied) with a scaling variable s, while the relaxation time was divided by s1.8 (Fig. 5).

FIG. 5.

Scaled relaxation time as a function of a scaled Tabor parameter for different power law indenters and interfacial dimensions. Open and filled symbols refer to D = 1 and D = 2, respectively. Moreover, n = 1 (blue circles), n = 2 (orange squares), n = 3 (green diamonds), and n = 4 (red triangles). The dashed, gray line shows the power law (sμT)1.8.

FIG. 5.

Scaled relaxation time as a function of a scaled Tabor parameter for different power law indenters and interfacial dimensions. Open and filled symbols refer to D = 1 and D = 2, respectively. Moreover, n = 1 (blue circles), n = 2 (orange squares), n = 3 (green diamonds), and n = 4 (red triangles). The dashed, gray line shows the power law (sμT)1.8.

Close modal

It remains to be discussed to what degree our results depend on the precise form of the cohesive-zone model (CZM). To address this issue, we repeated some simulations using a Dugdale model33 and found the same τμT1.8 scaling law as when using Eq. (2). Prefactors of the scaling laws cannot be compared directly because the length scale used in the definition of the Tabor parameter can be either the literal range of adhesion ρ or the ratio of surface energy and maximum tensile stress. Taking the geometric mean of those two options makes the Dugdale potential relax roughly 15% more slowly than the default CZM with the same Tabor parameter. We attribute the slight increase in relaxation time and thus dissipation by the Dugdale model to the discontinuity of the CZM at the cutoff. It leads to a diverging second derivative, which in turn induces enhanced local surface velocity for a moving crack and thus enhanced velocity gradients in the material and increased total dissipation compared to more smoothly evolving CZMs.

In this work, we confirmed numerically that the crack closure dynamics of indenters with power law profile in contact with an adhesive, linearly viscoelastic foundation has a universal behavior, at least at the late stages of the contact formation process when the contact radius has grown to a size that adhesion can be labeled short-ranged. Analysis of the final stages of the contact formation reveals that the relaxation times increase approximately with the inverse range of adhesion to the power of 1.8. Since Tabor parameters can be quite large in practical applications, this means that crack closure can last rather long times. To give an admittedly extreme example, assuming E* = 10 MPa, γ = 40 mJ/m2, R = 20 μm, and a range of adhesion typical for Lennard-Jones interactions, say ρ = 3.5 Å, yields μT = 195. Thus, using the data for D = n = 2 in Table I, we obtain τ/τMxw ≈ 83 · (195/3)1.8 ≈ 0.15 · 106. Making the link to real viscoelastic materials is challenging, because they have a broad distribution of relaxation times, which are quite sensitive to temperature and materials composition. This in turn makes it difficult if not impossible to state a generally valid numerical value for τMxw. However, if a dynamical analysis is known, an upper estimate for τMxw should be given by the equation E″(1/τMxw) = E0 on the small-frequency branch of the loss modulus.

Unfortunately, it is not clear to what degree the scaling might be affected by small-scale roughness. In the extreme case, there will be contact line pinning due to elastic multistability, which can be caused by structural heterogeneity.14 In this case, our estimates would only imply a crude lower bound for the contact formation time. A hint in this direction comes from previous simulations.8 They mimicked successfully dynamical experiments on the adhesion between an elastomer and a flat punch to which (single-sinusoidal) small-scale roughness was added. In that work, we had identified a steeper dependence of relaxation times on the range of adhesion than in the present work, although our old estimate was based on an analysis, which was much less systematic than the one presented here.

The authors have no conflicts to disclose.

C. Müller: Conceptualization (equal); Data curation (lead); Formal analysis (equal); Investigation (lead); Methodology (equal); Software (lead); Writing – original draft (supporting); Writing – review & editing (equal). M. H. Müser: Conceptualization (equal); Formal analysis (equal); Methodology (equal); Supervision (lead); Writing – original draft (lead); Writing – review & editing (equal).

The data that support the findings of this study are available from the corresponding author upon reasonable request.

While the contact mechanics of both short-range30 and finite-range32 adhesive power law indenters have been solved, it might be beneficial to have simple arguments allowing one to estimate pull-off forces, work of adhesion, and Tabor parameters in simple terms up to prefactors of order unity without having to embark on the high level of complexity pioneered by Maugis.34 For this purpose, it is helpful to realize that the crack closure dynamics for a given E(ω) can only depend on the dimensionless numbers describing the problem, i.e., n and μT. In the following, we derive an expression, which, up to constants of order unity, gives the generalized Tabor parameter. To this end, we define μT such that μT ≡ 1, when simple estimates for the stress-standard deviation in the limit of short-range adhesion match the maximum tension for finite-range adhesion. Our treatment also allows us to identify scaling relations for power law indenters. While similar relations can be deduced from existing literature, we believe our derivation to be original while requiring close to the least possible amount of prior background on contact mechanics and graphite, chalk, ink, or toner in order to arrive at generally valid scaling relations.

For a given shape (shp) of the displacement field, be it the zero-load (zl) or the pull-off (po) shape, the elastic energy Uel in areal contacts (D = 2) or its line density uel ≡ ΔUelLy in line contacts (D = 1) can only be of the form
(A1a)
(A1b)
in the limit of short-range adhesion. Here, a is the contact radius, while the gn,Dshp are constants that depend on the exponent n, the interfacial dimension D, and on the shape of the displacement field. The corresponding total surface energy Us or line density us gained on making contact are
(A2a)
(A2b)
Eliminating h(a) with the help of Eq. (1) and minimizing the total energy in the load-free case w.r.t. a yield a zero-load radii of
(A3)
For the surface of a semi-infinite solid, the stress variance is nothing but Δσ2=(E*/2)2(u)2, where ⟨⋯⟩ denotes spatial average. This relation is heavily exploited in Persson’s contact mechanics theory for the contact mechanics of randomly rough contacts. However, it also turns out useful for deterministic tip shapes, in particular power law indenters, when restricting the spatial average over the true contact. Since the mean-square height gradient ḡc2 averaged over the contact satisfies
(A4)
the stress variance in the limit of short-range adhesion is roughly on par with the square of the maximum tension if
(A5)
where we suppressed all numerical prefactors, which are deemed to be usually of order unity. We define the Tabor parameter to be unity for the range of adhesion satisfying Eq. (A5) so that
(A6)
which is identical to Eq. (5).
As a side comment, we note that our scaling analysis also allows the pull-off force Fpo and the work of adhesion Wpo in D = 2 and their corresponding line densities using lower-case letters in D = 1 to be estimated. To this end, we assume that the mean contact stress at pull-off scales linearly with the stress-standard deviation at zero load. Thus, Fpoa02E*ḡc for D = 2 while fpoa0E*ḡc for D = 1 so that
(A7a)
(A7b)
which satisfies well-known relations like FpoγR for a regular Hertzian geometry (n = 2, D = 2) or FpoE*γR3 for a regular flat punch (n, D = 2). The work of adhesion of a power law indenter can only scale as the product of surface energy and (zero-load) contact area so that
(A8a)
(A8b)
Thus, the work of adhesion for a flat punch in D = 1 and D = 2 alike is the same when conducted very slowly or very quickly, i.e., when probing it with the high- or the low-frequency modulus, but it would be large at intermediate pull-off velocities, as argued, for example, in Ref. 26.
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