Introduction

The nature of glass is one of the most puzzling and challenging problems in condensed matter physics. One crucial aspect is the complex relaxation behaviors that arise from nonequilibrium thermodynamics. When glasses are subjected to external stimulations, e.g. stress or elevated temperatures, they usually relax monotonically towards lower energy states1,2,3,4. But some anomalous nonmonotonic relaxations may happen under multi-step annealing, which was observed by Kovacs in the 1960s5. Since then, the enthalpy/volume rejuvenation phenomenon after two-step annealing is also known as the Kovacs memory effect5,6. Such memory effect is revealed to be related to the heterogeneous nature of glasses7,8, which can be described by phenomenological models such as the Tool-Narayanaswamy-Moynihan (TNM) model2,6,9,10,11,12,13,14, and is closely related to the complex relaxation paths in the deep aging stage15. Thus, studying complex relaxation behaviors is of vital importance for understanding the non-equilibrium nature of glasses.

Besides the classical Kovacs memory effect in structural glasses that are triggered by the multi-step thermal annealing process15,16,17,18,19,20, the Kovacs-like memory effect has been widely observed in other complex disordered systems14,21,22,23,24,25,26. Multistep mechanic stimulation can trigger the memory effect in the disordered granular system, crumpled thin sheets, and elastic foams2,14,18,23,27,28. Multistep thermal and magnetic stimulations can trigger the memory effect in disordered magnetic nanoparticles21,29,30. For structural glasses, recent results suggest that the stress and the thermal effects both contribute similarly to triggering flow31,32,33. However, the mechanic-field-triggered memory effect has been rarely observed in structural glasses21. It is intriguing to study whether structural glasses exhibit Kovacs-like memory effect under multiple strain stimulations.

In this Letter, we report a Kovacs-like memory effect in structural glasses, which is triggered by the two-step strain-stimulating procedure. This phenomenon is probably universal in glasses as it is observed in two metallic glasses (MGs) and a polymer glass (Polyvinyl chloride, PVC) with distinct properties. The influence of applied strains, temperatures, and preloading times have been systematically studied, and the relationship between the memory effect and relaxation kinetics is unveiled. In-situ high energy X-ray diffraction is applied to unravel the micro-structure origin of the memory effect.

Results

Figure 1a illustrates the two-step tensile protocol, starting with an initial strain \({\varepsilon }_{0}=0\). Subsequently, the strain holds at a preloading strain of \({\varepsilon }_{1}\) for time tw and then jumps to another stress-relaxation strain of \({\varepsilon }_{2}\). Figure 1b shows the representative stress relaxation curves for Ti16.7Zr16.7Hf16.7Cu16.7Ni16.7Be16.7 high-entropy MG with \({\varepsilon }_{1}=0.5\% \) at a tested temperature Ta = 593 K. The dynamic characterization is presented in Supplementary Fig. 1. During the preloading step, the stress decays monotonically as expected. In the second step, when \({\varepsilon }_{2}\) > \({\varepsilon }_{1}\), the stress continues to decay monotonically. However, when \({\varepsilon }_{2}\) < \({\varepsilon }_{1}\), the stress increases first and then decreases after reaching a maximum. Such a non-monotonic change in stress is analogous to the classical Kovacs memory effect of enthalpy/volume induced by low- to-high two temperatures annealing5,34. For the same \({\varepsilon }_{1}\), a smaller \({\varepsilon }_{2}\) gives a stronger stress rejuvenation. The anomalous nonmonotonic evolution in stress, here named the stress memory effect, is also observed in two other glasses with distinct chemical compositions, (Fe11Zr1)91.2B8.8 MG and Polyvinyl chloride (PVC), as shown in Fig. 1c. The three representative glasses cover a wide range of physical properties, e.g., glass transition temperature, fragility, and yield strength, suggesting that such a stress memory effect is probably a universal characteristic of glasses.

Fig. 1: Two-step strain annealing protocol and stress memory effect.
figure 1

a The schematic of tensile stress relaxation with two different applied strains (\({\varepsilon }_{1}\), \({\varepsilon }_{2}\)) with an initial strain ε0 = 0. The preloading time is tw. F represents axial tensile force. The blue gradient represents increasing strain, while the red gradient represents decreasing strain. b The stress relaxation curves of two-step strain stimulations (\({\varepsilon }_{1}=0.5\%\), \({\varepsilon }_{2}=0.2\%\sim 0.6\%\)) for TiZrHfCuNiBe metallic glass at Ta = 593 K. c The semi-logarithmic plots of non-monotonic stress relaxation curves for three glasses (Red: TiZrHfCuNiBe high-entropy MG with the preload parameters of (\({\varepsilon }_{1}=0.5\%\), \({\varepsilon }_{2}=0.3\%\), tw = 900 s, Ta = 593 K); Black: (Fe11Zr1)91.2B8.8 MG with the preload parameters of (\({\varepsilon }_{1}=0.4\%\), \({\varepsilon }_{2}=0.2\%\), tw = 1800 s, Ta = 597 K); Blue: PVC with the preload parameters of (\({\varepsilon }_{1}=0.5\%\), \({\varepsilon }_{2}=0.3\%\), tw = 300 s, Ta = 318 K)). The titles of all three y-axis are σ (MPa). The tp and Δσ denote the peak time and the strength of the memory effect, respectively. Source data are provided as a Source Data file.

The influence of preloading strain \({\varepsilon }_{1}\) and annealing temperature on the stress memory effect are summarized in Fig. 2. Figure 2a shows stress evolution in the second iso-strain stage for different pre-loading strains \({\varepsilon }_{1}\). The memory strength \(\Delta \sigma\) and the peak time tp increase when the pre-loading strain increases, as shown in Fig. 2a–c. Figure 2d shows the stress memory effect in the second iso-strain stage at different temperatures Ta. The peak time tp increases with temperature (see Fig. 2e). The memory strength \(\Delta \sigma\) also increases with temperature and increases faster at higher temperatures, as shown in Fig. 2f. The nonmonotonic normalized stress can be well fitted by double Kohlrausch-Williams-Watts (KWW) expression3,35,36:

$$\frac{\sigma (t)}{{\sigma }_{0}}=A\cdot \exp \left(-{\left(\frac{{t}^{{\prime} }}{{\tau }_{1}}\right)}^{{\beta }_{1}}\right)+(1-A)\cdot \exp \left(-{\left(\frac{{t}^{{\prime} }}{{\tau }_{2}}\right)}^{{\beta }_{2}}\right)$$
(1)

where \(\sigma \left(t\right)\) and \({\sigma }_{0}\) represent the immediate and initial stress in the second stage, respectively; t’ = t-tw is the time in the second stage; τ1 and τ2 are the characteristic relaxation times; β1 and β2 are the stretching exponents describing the non-exponential behavior of the relaxations. A and 1-A reflect the corresponding relaxation intensity. The fitted relaxation time is shown in Supplementary Fig. 3.

Fig. 2: Influences of the preloading strain and temperature on stress memory effect for TiZrHfCuNiBe high-entropy MG.
figure 2

a The stress memory effect for different preloading strains \({\varepsilon }_{1}\). The dependence of b peak time tp and c the strength of memory effect \(\triangle \sigma\) on \({\varepsilon }_{1}\). d The stress memory effect at different annealing temperatures Ta. The dependence of e peak time tp and f the relative strength of memory effect \(\triangle \sigma /{\sigma }_{0}\) on Ta. The solid curves correspond to double KWW fitting. Error bars represent standard deviations. Source data are provided as a Source Data file.

The influence of the pre-loading time tw on the stress memory effect is studied for three representative glasses, as shown in Fig. 3a–c. The dependence of the memory strength \(\Delta \sigma\) on pre-loading time is shown in Fig. 3d–f. Generally, the \(\Delta \sigma\) increases monotonically as the preloading time increases. It is interesting to note that there exists a critical time, before which the \(\Delta \sigma\) is very small, but after which the \(\Delta \sigma\) increases sharply. This is a notable result of the stress memory effect, which has not been reported in disordered granular systems.

Fig. 3: Evolution of stress memory effect with annealing time for three glasses.
figure 3

a TiZrHfCuNiBe high-entropy MG at 593 K with \({\varepsilon }_{1}=0.5\%\) and \({\varepsilon }_{2}=0.3\%\), b (Fe11Zr1)91.2B8.8 MG at 597 K with \({\varepsilon }_{1}=0.4\%\) and \({\varepsilon }_{2}=0.2\%\), and c PVC polymer glass at 318 K with \({\varepsilon }_{1}=0.5\%\) and \({\varepsilon }_{2}=0.3\%\). The solid curves correspond to KWW fitting. The strength of the memory effect (\(\Delta \sigma\)) as a function of tw are shown in df accordingly. The blue shaded area highlights the fast increase of memory strength \(\Delta \sigma\). Error bars represent standard deviations. Source data are provided as a Source Data file.

Discussion

To study the physical origin of the emerging stress memory effect, the relaxation activation energy \({E}_{a}\) during the preloading stage was calculated according to the KWW and Arrhenius equations3,37,38 (see details in section 4 of Supplementary information). The time-dependent \({E}_{a}\) for the three representative glasses during the preloading step are shown in the upper panels of Fig. 4a–c. Considering Figs. 3 and 4, the Ea is small and does not change much with relaxation time while the stress memory effect is weak. When the relaxation time is long enough where the stress memory becomes strong, the Ea increases fast. The analogous change in Ea during isothermal annealing was reported in different glasses35,39,40,41, and it is attributed to the increased atomic collectivity during relaxation.

Fig. 4: Relaxation kinetics.
figure 4

Evolution of (Top) the activation energy \({E}_{a}\) and (Bottom) the fraction of strain recovery (\({1-\varepsilon }_{{vp}}/{\varepsilon }_{1}\)) with tw for a TiZrHfCuNiBe MG, b (Fe11Zr1)91.2B8.8 MG, and c PVC polymer. The experimental condition for strain recovery tests: Ti-MG (Ta = 593 K, \({\varepsilon }_{1}\) = 0.5%), Fe-MG (Ta = 597 K, \({\varepsilon }_{1}\) = 0.4%), and PVC (Ta = 318 K, \({\varepsilon }_{1}\) = 0.5%). (Calculation details for the activation energy and fraction of strain recovery are presented in sections 4 and 5 of Supplementary information). Source data are provided as a Source Data file.

Furthermore, we studied the strain recovery behavior after the preloading, see Supplementary Fig. 7. Below the glass transition temperature Tg, the mechanical response of the glassy system usually includes the instantaneous recoverable elastic strain \({\varepsilon }_{{el}}\), slow recoverable anelastic strain \({\varepsilon }_{{an}}\), and irrecoverable viscoplastic strain \({\varepsilon }_{{vp}}\), as distinguished in Supplementary Fig. 7a. The fraction of strain recovery (\({1-\varepsilon }_{{vp}}/{\varepsilon }_{1}\)) of three glasses after various preloading times tw are shown in the lower panels of Fig. 4. When the tw is short, the glasses exhibit complete strain recovery. When the tw is long enough where stress memory thrives, the glass cannot recover completely, which suggests irreversible configuration during the preloading process42. The reversible process is clearly associated with the small Ea (see the upper panels of Fig. 4), and it should be related to the activation and motion of localized soft domains that are constrained by the elastic matrix40,41,42,43,44. As for the long-time annealing, the irrecoverable viscoplastic strain emerges associated with the sharp increase in Ea, and it derives from the percolation and cooperative motions of soft domains42,45. The fast and slow relaxation processes can be identified respectively as \(\beta\) process and collective motion39,40,42,46.

To unravel the structural origin of the stress memory effect, we utilize high energy synchrotron X-ray diffraction to investigate the atomic scale structural changes in TiZrHfCuNiBe MG during the stress memory effect, and the experimental technical details are displayed in Supplementary Fig. 8. Figure 5a, c shows the reduced pair distribution functions G(r) of TiZrHfCuNiBe MG during the preloading stage and during the memory stage, respectively (stress evolution curve shown in Supplementary Fig. 8c). Close inspections indicate that the first nearest neighbor shell split into two sub-peaks (insets in Fig. 5a, c), in which the left sub-peak corresponds to the shorter inter-atomic band lengths dominated by small-size atoms, while the larger atoms dominate the right sub-peak46,47,48. According to the interatomic bond lengths and weight factors provided in Supplementary Table 1, the left sub-peak at approximately 2.70 Å can be primarily attributed to the Hf-Cu and Hf-Ni atomic pairs, while the right sub-peak at around 3.10 Å is mainly dominated by the Zr-Hf, Hf-Hf, and Ti-Hf atomic pairs. As the stress decays, the full width at half maximum (FWHM) of the first G(r) peak decreases (Fig. 5b), together with the left-shifted peak position, it suggests that the atomic packing becomes denser at a longer time47. But when stress increases during the memory stage (Fig. 5d), the FWHM increases and the peak position shifts to the right-hand side. This suggests that the atomic packing in the short-range becomes loose.

Fig. 5: Structural origin of stress memory effect for the TiZrHfCuNiBe high-entropy MG at 593 K.
figure 5

a The reduced pair distribution function G(r) in the stress decreasing stage during pre-loading at a fixed strain of 0.5% and b the corresponding evolution of the full width at half maximum (FWHM) of the first peak. c The evolution of G(r) during the memory stage with \({\varepsilon }_{2}\) = 0.3% (after \({\varepsilon }_{1}\) = 0.5% and tw = 900 s) and d the corresponding evolution of FWHM of the first peak. The insets show the zoomed-in data of the corresponding nearest neighbor atomic diffraction peaks. e The correlation between the memory peak time tp and the recovery characteristic time \({\tau }_{{rec}}\). The square, triangle, and circular symbols represent data measured at different preloading variables of temperature, strain, and time, respectively. The data of peak time tp are taken from Fig. 2 and Supplementary Fig. 2. The blue solid straight line represents the linear fitting of tp = -630.4 + τrec, with a high regression coefficient of R2 = 0.99. f The schematic illustration for the evolution of atomic packing structure for anelastic stress relaxation and recovery (memory) process. Source data are provided as a Source Data file.

The anelastic recovery tests under the various preloading conditions in TiZrHfCuNiBe MG were performed to investigate the reversible contribution to the deformation, as illustrated in Supplementary Fig. 9. The anelastic recovery process can be fitted by the KWW equation: \(\frac{{\varepsilon }_{{an}}\left(t\right)-{\varepsilon }_{{an}}\left(\infty \right)}{{\varepsilon }_{{an}}\left(0\right)-{\varepsilon }_{{an}}\left(\infty \right)}= \exp (-{(\frac{t}{{\tau }_{{rec}}})}^{{\beta }_{{rec}}})\)37,39. The relaxation characteristic time \({\tau }_{{rec}}\) reflects the timescale of the anelastic recovery3,42,46,49. The \({\varepsilon }_{{an}}\left(\infty \right)\) represents the ultimate strain achieved at the end of the anelastic recovery, and \({\beta }_{{rec}}\) is a stretching exponent. The fitting curves for various temperatures Ta, preloading strains \({\varepsilon }_{1}\) and times tw are shown in Supplementary Fig. 9. Figure 5e confirms a linear relationship between the peak time tp and the recovery characteristic time \({\tau }_{{rec}}\) over several decades. This indicates that the stress memory effect originates from the recovery of reversible anelastic components.

Figure 5f shows a schematic illustration of the local atomic arrangement for reversible events in stress relaxation. As the strain increases \(({\varepsilon }_{{{{{{{\rm{I}}}}}}}}\to {\varepsilon }_{\Pi })\), the atoms pack more densely. This reconfiguration arises from the diffusion of small atoms within the network formed by the large solvent atomics, and it can be related to the left shift of the first sub-peak (Fig. 5a). During the memory stage when unloading to a lower strain \(({\varepsilon }_{\Pi }\to {\varepsilon }_{{{{{{\rm{{I}}}}}}}})\), the small atoms move toward a looser configuration according to the right shift of the first sub-peaks (Fig. 5c). This observation coincides with the atomic mechanisms of the dynamic process in \(\beta\) relaxation47,50. This result indicates that the stress memory effect arises from reversible \(\beta\) relaxations.

Recent evidence has stated that the rejuvenation of glasses could be induced by the mismatch of the thermal expansion coefficient or the modulus fluctuation between neighboring local domains51,52,53 when subjected to the same external perturbation. For the stress memory effect, as the applied strain jumps to a lower value, the mismatch of momentary modulus between neighboring local domains produces internal stresses, which would induce an inverse process and increase the stress. Longer preloading can stimulate abundant internal stress and facilitate more runback of reversible β events upon unloading, which generate a more pronounced stress memory effect in the collective motion process (see Fig. 3). This aligns with the thriving of the Kovacs memory effect in a deep aging state characterized by a large activation entropy15. The herein reversible β events also support the rational presence of the reversible faster relaxing element in the phenomenological Amir–Oreg–Imry (AOI) model1,2, which has been widely used to explain the nonmonotonic relaxation phenomenon2,22,23,54.

The classical Kovacs memory effect has a typical three-temperature protocol5,6,19,25,34,55, say \({T}_{0}\), \({T}_{2}\) and \({T}_{1}\), where \({T}_{0}\) is the initial equilibrated temperature, \({T}_{1}\) and \({T}_{2}\) are annealing temperatures. The Kovacs memory effect happens only as \({T}_{0} > {T}_{2} > {T}_{1}\), while herein the stress memory effect happens only \({\varepsilon }_{0} < {\varepsilon }_{2} < {\varepsilon }_{1}\). Inspired by the theoretical works of Prados et al.14,19,26, the contribution of the temperature perturbation to the glass system is alike to the stress/strain by considering \(\beta E\propto \beta \sigma \varepsilon\). Here \(\beta=\frac{1}{{k}_{B}T}\), and \({k}_{B}\) is the Boltzmann constant. \(E\) represents the energy, which is basically proportional to \(\sigma \varepsilon\)19. Then, we can understand the effect of applied strain \(\varepsilon\) on the glass system as a perturbation \(\beta\) in the Kovacs memory effect. For instance, the low-to-high temperature annealing leads to a decrease in \(\beta\), which is equal to the stimulation of high-to-low strain annealing in the protocol under a fixed temperature (Fig. 1a). The convergence of the two memory effects stems from their common structural origin, as the classical Kovacs memory effect also may arise from the recovery of reversible loosely packed regions56,57.

In conclusion, we have observed a Kovacs-like stress memory effect when glasses are stimulated by high-to-low two-step strain stimulations. The stress memory only appears when the second-step strain is smaller than the first-step strain. Larger applied strain, longer stimulation time in the first stage, and higher temperature make the memory effect stronger. The runback of reversible motions of small atoms is the essential mobilizing mechanism of the memory effect, which is confirmed by the reconfiguration of short-range atomic packing structures.

Methods

Sample fabrication

The master alloys of Ti16.7Zr16.7Hf16.7Cu16.7Ni16.7Be16.7, (Fe11Zr1)91.2B8.8 (at%) were prepared by arc melting. The metallic glass ribbons with a thickness of approximately 30 μm were fabricated by the melt spinning with a tangent velocity of approximately 40 m/s. Polyvinyl chloride films with a thickness of approximately 150 μm were purchased from the manufacturer.

Dynamic characterization

The dynamical mechanical behavior of the three glasses was measured using the dynamic thermomechanical analysis apparatus (TA-DMA Q800). The mechanical spectroscopy measurements were performed at a heating rate of 5 K/min with a driving frequency of 1 Hz.

Stress-relaxation and strain-recovery measurements

Isothermal stress relaxation tests were performed on a TA DMA-Q800 instrument using one or two-step protocols (see Fig. 1a) at target temperatures. Subsequently, the strain recovery tests were conducted by unloading the stress after the relaxation period.

Structural characterization

The local structural characterization was performed in China’s Beijing synchrotron radiation facility. The in-situ experiments were conducted in the synchrotron X-ray beam at 3W1, which utilized monochromatic synchrotron radiation with a wavelength of 0.2065 Å (energy of 60.037 keV). The diffraction experiments were carried out in the Debye-Scherrer geometry. The layout of the experimental setup is shown in Supplementary Fig. 8a. The incident beam had a well-collimated cross-section of 0.8\(\times\)0.8 mm². Diffraction patterns were collected using an iRay Mercu 1717HS image plate detector, which had a resolution of 3072\(\times\)3072 pixels, with each pixel corresponding to a size of 139\(\times\)139 µm². The detector was carefully positioned orthogonal to the x-ray beam, and the distance between the 2D detector and the sample was adjusted to about 280 mm in terms of covering a high-Q range up to 16.5 Ź (where \(Q=4\pi \sin \theta /\lambda\)). θ is half the scattering angle, and λ is the incident wavelength. The samples were exposed to the incident beam for 5 s during the experiments. Each total diffusion pattern was fully integrated to achieve the diffraction data and the Fourier transformations from I(\(Q\)) to \(G\left(r\right)\) were conducted using the PDFgetx3 program with the following equation48:

$$S\left(Q\right)=1+\frac{{I}_{e}\left(Q\right)-\left[\mathop{\sum }\limits_{i=1}^{n}{c}_{i}{f}_{i}^{2}(Q)\right]}{\left[\mathop{\sum }\limits_{i=1}^{n}{c}_{i}{f}_{i}^{2}(Q)\right]}, $$

and \(G\left(r\right)=\frac{2}{\pi }{\int }_{0}^{{Q}_{\max }}Q\left(S\left(Q\right)-1\right)\sin \left({rQ}\right){dQ}\).

Where \({I}_{e}\left(Q\right)\) represents the normalized elastically scattered intensity, and \(r\) denotes the radial distance. \({c}_{i}\) and \({f}_{i}(Q)\) refer to the atomic concentration and the scattering factor of ith atomic in the tested alloy. The weighting factor of i-j atoms pair was calculated according to the following manner48:

$${w}_{{ij}}=\left\{\begin{array}{c}\frac{2{c}_{i}{c}_{j}{f}_{i}(0){f}_{j}(0)}{{\left[\mathop{\sum }\limits_{k=1}^{n}{c}_{k}{f}_{k}(0)\right]}^{2}},{i}\ne j\\ \frac{{c}_{i}^{2}{f}_{i}^{2}(0)}{{\left[\mathop{\sum }\limits_{k=1}^{n}{c}_{k}{f}_{k}(0)\right]}^{2}},{i}=j\end{array}\right..$$

The specimens of amorphous ribbon were subjected to tension using the Linkam TST350 straining system. Supplementary Fig. 8b shows the loading protocol for tensile stress relaxation with two different applied strains (\({\varepsilon }_{1}=0.5\%,{\varepsilon }_{1}=0.3\%\)) at a temperature of 593 K. The tensile strain was increased in increments of 200%/min, and the gauge length of Linkam TST350 was 40 mm. The stress evolution corresponding to the two-step process is shown in Supplementary Fig. 8c.

Reporting summary

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