- The paper demonstrates that guided SH₀, S₀, and A₀ wave dispersion probes different derivatives of strain energy, exposing constitutive information that uniaxial stress–strain data cannot reveal.
- Wave measurements distinguish Mooney–Rivlin, Gent–Thomas, and Carroll models at small-to-moderate strains, while augmented Carroll and Gent–Thomas models generally outperform alternatives in the strain-hardening regime.
- The method cannot distinguish Gent- and Dobrynin–Carrillo-based limiting-chain models, and its conclusions are partly affected by clamp-induced biaxiality and the fitted viscoelastic coupling parameter β′.
Motivation and scope
Identifying a constitutive law for rubber-like solids that remains valid across all deformation classes and the full range of achievable extensions is a long-standing problem in nonlinear elasticity. The difficulty is well documented: Ogden and collaborators showed that multiple parameter sets can fit uniaxial tension data equally well while yielding markedly different predictions for other deformations, and Destrade et al. later formalized a fitting procedure that yields a unique optimum for simple extension data while emphasizing that static uniaxial tests alone cannot discriminate among constitutive models sharing a common structure. The paper under review proposes an alternative source of information: incremental guided elastic waves propagating in an elastomer plate subjected to large static uniaxial extension (2603.18839). The central claim is that dispersion measurements of the three zero-order guided modes reveal sensitivities of the strain-energy density that are invisible in the corresponding stress–strain curve, thereby lifting some—but not all—of the degeneracy between hyperelastic models.
Experimental characterization of guided modes
The experiments extend prior work on Ecoflex OO-30 plates (60 cm × 3 mm) held vertically between clamps, where in-plane SH0 and S0 mode dispersions were measured via stroboscopic imaging and digital image correlation for stretches λ∈[1.03,2.27]. The new contribution adds the flexural A0 mode, measured on a 2.5 mm-thick plate using a shaker-driven line source emitting a quadratic chirp (200 Hz down to 1 Hz) and a laser-sheet deflection technique recorded at 1 kHz. Dispersion relations are extracted from two-dimensional Fourier transforms of the displacement fields.
Two experimental caveats matter for the interpretation. First, the imposed deformation is not strictly uniaxial: marker tracking gives λ3=λ−0.41 (in-plane sample) and λ−0.39 (out-of-plane sample), because the clamps constrain lateral contraction; gravity also produces a small pre-stretch (λ=1.03 at rest). Second, the A0 mode proves highly sensitive to stretch: it rapidly departs from its parabolic long-wavelength shape and becomes nearly non-dispersive parallel to the elongation at large λ, whereas the in-plane mode velocities increase along the stretch direction (string-like tension behavior) and are barely affected perpendicular to it.
Modelling framework
The theoretical pipeline combines three ingredients: (i) nearly incompressible hyperelastic strain-energy densities written as deviatoric plus volumetric parts, compatible with fourth-order weakly nonlinear elasticity; (ii) acoustoelastic theory for incremental motions superposed on the finite deformation, with viscoelasticity incorporated through a fractional Kelvin–Voigt model (μ=μ0(1+(iωτ)n), with S00s and S01 from rheometry), introducing a coupling parameter S02 between viscosity and pre-stress; and (iii) long-wavelength approximations for the phase velocities of the S03, S04, and S05 modes, supplemented by a semi-analytical spectral collocation scheme solving for complex wavenumbers—necessary to capture the full S06 dispersion, which the long-wavelength formulas fail to reproduce beyond a limited wavenumber range.
The key structural insight is that different modes probe different derivatives of S07. In the long-wavelength limit, S08 velocities relate to first derivatives of S09 (equivalently, the stress difference λ∈[1.03,2.27]0, independent of rheology), the λ∈[1.03,2.27]1 velocities equal λ∈[1.03,2.27]2 and λ∈[1.03,2.27]3 directly, while the λ∈[1.03,2.27]4 velocity depends on second-order derivatives of λ∈[1.03,2.27]5 with respect to the principal stretches—the derivative of stress with stretch. This hierarchy explains why the pseudo-longitudinal mode amplifies minute differences between constitutive laws that fit the static curve identically. The price paid is the extra parameter λ∈[1.03,2.27]6, which must be determined from dynamic data itself.
Discriminating the λ∈[1.03,2.27]7 term: small to moderate strains
Following Destrade et al.'s procedure, the authors identify the extent of the small-to-moderate regime via the maximum relative residual in Mooney space, finding a sharp error increase beyond λ∈[1.03,2.27]8. Three two-parameter models differing only in the functional form of the λ∈[1.03,2.27]9-dependent term—Mooney–Rivlin, Gent–Thomas, and Carroll—are fitted to the uniaxial data. All three fit the Mooney plot excellently and yield essentially identical shear moduli (A00–23.4 kPa), confirming that the static test cannot discriminate them.
The wave data can. At fixed frequency (170 Hz for in-plane modes, 50 Hz for A01), the predicted phase velocity of the A02 mode propagating perpendicular to the stretch differs measurably between the three models even within the fitted range, with Mooney–Rivlin performing best. Notably, A03 is recovered for all three models in this regime, indicating that viscous effects do not couple to pre-stress at moderate elongations—in contrast with the non-zero value reported in earlier work covering larger stretches.
Strain-hardening regime
To capture the upturn in the Mooney plot (A04 up to 2.5), a power-law term proportional to A05 with A06 is appended to each model. All augmented models superimpose almost perfectly on the static data, again leaving the Mooney plot non-discriminating. The dynamic comparison is more informative: the maximum relative velocity error across all modes and directions is 12.7% for Carroll+A07, 16.9% for Gent–Thomas+A08, but 23.7% for Mooney–Rivlin+A09, with the largest Mooney–Rivlin error occurring for the λ3=λ−0.410 mode perpendicular to the stretch. This failure is traced to the fact that this mode's velocity equals λ3=λ−0.411: the clamped geometry imposes a slightly biaxial stress state (λ3=λ−0.412), a deformation class where Mooney–Rivlin is known to perform poorly. The authors state plainly that had the deformation been strictly uniaxial, the λ3=λ−0.413 mode would not be discriminating—and excluding it drops the Mooney–Rivlin error to 7.0%, the best of the three. This is a genuine caveat on the claimed discrimination: part of it stems from the imperfect boundary conditions rather than from intrinsic model ranking. The coupling parameter becomes non-zero in this regime (λ3=λ−0.414–0.32) but is only weakly dependent on the choice of constitutive law, so conclusions are robust to its determination.
For the limiting-chain regime, the authors fit the Gent model (freely jointed chain) and the Dobrynin–Carrillo model (worm-like chain), each augmented with a Gent–Thomas λ3=λ−0.415 term, using only three parameters. Both describe the full static curve and all measured phase velocities accurately, and—critically—their wave predictions are indistinguishable from each other, even extrapolated beyond the experimentally accessed range. Like their static counterparts, the dynamic measurements therefore cannot distinguish generalized neo-Hookean models representing different microscopic chain statistics. The practical recommendation is that these three-parameter models advantageously replace the four-parameter power-law constructions.
Limitations and open questions
Several limitations are acknowledged or implicit. The discrimination of λ3=λ−0.416 forms relies partly on the unintended biaxiality of the loading; a truly uniaxial setup would weaken the λ3=λ−0.417-based conclusion. Only first-order viscous terms in the pre-stress coupling are retained, an approximation the authors note may fail at large elongation where the response is strongly nonlinear. The value of λ3=λ−0.418 must be extracted from the same dynamic data used for validation, so it is not an independent prediction. The choice of comparison frequencies (170 Hz, 50 Hz) is admittedly arbitrary, though an interactive tool allows exploration over the full spectrum. Open questions left by the paper include whether higher-order guided modes (accessible, e.g., in strip geometries) provide richer discriminating information, whether attenuation measurements can constrain the hyperelastic–viscoelastic coupling beyond the single λ3=λ−0.419 parameter, and whether a full wave-based inversion of constitutive parameters—rather than the static-fit-plus-validation scheme used here—is feasible.
Conclusion
This work demonstrates that incremental guided-wave dispersion in a pre-stretched soft plate carries constitutive information absent from the uniaxial stress–strain curve: sensitivity to second derivatives of the strain energy (via the λ−0.390 mode) and to transverse stress (via the λ−0.391 mode). Guided-wave measurements lift the degeneracy among models with different λ−0.392 functional forms—favoring Gent–Thomas and Carroll forms overall—while remaining blind to differences among generalized neo-Hookean limiting-chain models. The results echo the classical lesson from multi-deformation-class static testing, obtained here from a single specimen geometry, and suggest that wave-based mechanical characterization could complement standard traction protocols for soft incompressible media (2603.18839).