In the following subsubsections, the fundamental physics and the governing constitutive equations are systematically detailed to establish a rigorous analytical framework. Starting from an adapted linear solid approach, by integrating the principles of continuum mechanics with polymer thermodynamics, the discussion progresses from the micro-scale interactions within the PLA/PCL blends to the formulation of a comprehensive theoretical model. This mathematical derivation aims to fully capture the underlying mechanisms of the shape-memory effect, accurately describing both the shape-fixing and shape-recovery stages that define the material’s functional response.
2.4.1. Adapted Standard Linear Solid Model for Shape Memory Polymers: Theoretical Framework
The macroscopic thermomechanical behavior of the PLA/PCL blend is described by a constitutive differential equation derived from a modified Standard Linear Solid (mSLS) model (see
Figure 2). Deviating from conventional three-parameter viscoelastic frameworks [
27,
28], our model incorporates a thermal activation plastic-viscous strain element (
) in series with the primary elastic spring (
E1), according to a four-element configuration involving a slip mechanism proposed by Tobushi et al. [
29]. Specifically, this element remains dormant when the temperature is below the glass transition temperature
Tg or the internal stress does not meet the yielding condition. Conversely, it is triggered once the temperature exceeds
Tg and the driving stress surpasses the temperature-dependent yield threshold (
σy).
The proposed rheological model effectively captures the thermomechanical response of the PLA/PCL blends under investigation. This architecture enables a direct representation of the ‘frozen’ strain within the PLA matrix by decoupling stored entropic energy from the dissipative mechanisms inherent to the PCL phase. Specifically, the upper branch serves as the material’s ‘elastic skeleton,’ representing the memory effect and matrix elasticity of the continuous PLA phase; it physically accounts for the storage of elastic energy and the ability to fix a temporary shape, subsequently recovered via thermal activation above Tg. In parallel, the lower branch characterizes the viscoelasticity and damping properties of the PCL phase through a Maxwell element (E2 and η). This component captures viscoelastic chain sliding and the subsequent delayed mechanical response. Given its rubbery state at room temperature, the PCL phase enhances the blend’s dissipative capacity (η) and mitigates PLA brittleness, thereby governing the characteristic relaxation dynamics of the system.
The resulting analytical equation effectively captures the interplay between the macroscopic stress (
σ) and its first-order time derivative (
), correlating the elastic storage branches (
E1,
E2) with viscous dissipation (
η) and the temperature-dependent activation strain element (
εs), according to the following relationship:
where
and
denote the time derivatives of the total strain
ε and activation strains, respectively. Specifically,
represents the evolution rate of the internal state variable, capturing the kinetics of the strain storage and release mechanisms as the material crosses its transition temperature. See
Section S1 of the Supplementary Information for details about its mathematical derivation.
To simulate the complete shape-memory cycle, this general formulation is specialized into three distinct operational phases by applying specific boundary conditions and thermal constraints:
Shape Programming Phase—During the initial loading at
T >
Tg, a constant stress
σ0 rate is imposed on the specimen. In this regime, the thermal activation plastic-viscous element
εs is progressively engaged, allowing the primary elastic branch (
E1) to store the mechanical energy required for the subsequent recovery. The differential equation reduces to a linear growth form, where the material response is dominated by the simultaneous contribution of the elastic springs and the viscous dashpot, resulting in the linear increase in the deformation
ε. See
Section S1.1 of the Supplementary Information for mathematical details.
Cooling and Storage Phase—Once the maximum deformation
θmax is reached, the external stress is removed (
) while the temperature is rapidly decreased below
Tg. In this “dormant” state, a thermal activation function
α(
T,
χ), which is also dependent on the degree of crystallinity
χ, drops to zero, effectively “locking” the internal state variable (
εs) by nulling its evolution (
). At these temperatures, the high internal viscosity
η suppresses macromolecular relaxation, thereby preserving the programmed shape near its peak value, with only a marginal instantaneous elastic rebound occurring upon unloading. See
Section S1.2 of the Supplementary Information for mathematical details.
Shape Recovery Phase—Upon reheating the specimen above the activation threshold, the internal energy barrier is overcome, and the activation element is “unlocked” (
≠ 0). Under zero-stress conditions (
), the energy stored in the elastic branch E
1 during the programming phase is released, driving the strain recovery toward the permanent set
, where the effective relaxation time
dictates the recovery kinetics. See
Section S1.3 of the Supplementary Information for mathematical details.
In our theoretical setup, the sample is deformed into a U-shape. Under the assumption of Euler–Bernoulli beam theory, the surface strain
ε is proportional to the bending angle
θ. Consequently, the macroscopic response of the material can be modeled by substituting
ε with
θ in Equation (2). This approach treats the angular recovery as a direct proxy for strain recovery kinetics, assuming a geometric analogy between linear and angular deformation as follows:
where
Th is the sample thickness,
R is the radius of curvature, and
L is the length of the deformed segment. Given that
Th and
L remain constant during the test,
ε scales linearly with
θ (
).
2.4.3. Constitutive Material Parameters
Strategic calibration of the constitutive model relies on the integration of the intrinsic properties detailed in
Table 1. Beyond the general blend morphology, these specific thermo-viscoelastic parameters—primarily the glassy/rubbery moduli and glass transition temperatures—define the mechanical threshold of the networks. Moreover, thermal properties such as density (
ρ) and specific heat (
Cp) enable the model to account for the heat transfer dynamics within the composite beam. Collectively, these inputs allow the framework to accurately map molecular relaxation phenomena onto the observable shape-memory cycle of the PLA/PCL specimens. A comprehensive summary of the key parameters utilized in this study is provided in
Table S1 of the Supplementary Information, which includes additional details such as nominal values, symbols, units, variability ranges for the sensitivity analysis, and whether each parameter is derived experimentally, from literature, or via model calibration.
The effective thermophysical properties of the composite—specifically density (
), specific heat capacity (
), and degree of crystallinity (
)—were estimated via a linear rule of mixtures assuming a homogeneous phase distribution:
where
P represents the generic property, while
and
represent the weight percentage of the constituent polymers. For the crystalline fraction, the model was calibrated using experimental DSC benchmarks for the neat components (
χPLA = 14.3% and
χPCL = 42.6%, as reported in [
16,
17]), ensuring consistency at the compositional boundaries.
These linear refinements allow the model to predict the physical properties of intermediate biphasic compositions while consistently converging to the single-phase experimental benchmarks for or .
The effective glass transition temperature () of the switching phase was constrained within the 38–55 °C range to account for the partial miscibility of the PLA/PCL system. This rationale ensures high shape fixity (Rf); an activation threshold below this range would trigger premature chain mobility at ambient storage, leading to undesirable athermal recovery. The upper bound (55 °C) accounts for the PLA-rich phase Tg, marginally depressed by the PCL plasticizing effect, while the lower bound (38 °C) represents the stability threshold required to prevent spontaneous relaxation, consistent with the Tg plateau observed in partially immiscible biphasic blends.
Moreover, incorporating variable crystallinity into the thermomechanical framework accurately quantifies the reinforcing effects exerted by crystalline domains within both glassy and rubbery regimes. This approach successfully captures the evolution of Young’s modulus, thereby predicting the recovery kinetics and associated timescales of the shape-memory cycle.
Specifically, in this theoretical model, elastic moduli are modeled through a combination of the Voigt Rule of Mixtures—to capture the crystalline reinforcing effect in the glassy state—and an empirical crystallinity-based correction for the rubbery regime.
For the effective
χ-dependent glassy modulus
, the semi-crystalline blend is conceptualized as a heterogeneous system consisting of a high-stiffness crystalline phase (
Ec) and a compliant amorphous matrix (
Ea). Under the assumption of parallel mechanical coupling, the effective
χ-dependent glassy modulus
is expressed as:
The coefficients
and
represent the crystalline and amorphous moduli of PLA, while
and
refer to the respective phases of PCL. The values for these parameters were sourced from experimental data reported in our earlier work [
16] and are summarized as follows:
= 4.31 GPa,
= 266.4 MPa,
= 154 MPa, and
= 76.7 MPa.
Notably, the high values for the PLA crystalline phase (on the order of GPa) confirm that it serves as the primary structural component responsible for the mechanical stiffness of the hybrid system, whereas the PCL values reflect the rubbery nature of its amorphous phase at room temperature, ensuring the physical consistency between the model and the experimental setup. Given the significantly different orders of magnitude between these coefficients, the terms associated with the PCL phase could theoretically be neglected without substantial loss of accuracy. Nevertheless, these parameters are explicitly retained in our model to ensure physical completeness and to provide a comprehensive description of the mechanical contributions from both polymer components.
However, as highlighted in our previous study [
16], the experimental values for these parameters are susceptible to variations depending on the test working velocity.
Consequently, a comprehensive sensitivity and uncertainty analysis was performed by perturbing their nominal values Ec,nom and Ea,nom by ±5% and ±10%. This approach was carefully conducted to investigate the model’s stability and to assess how such experimental fluctuations propagate through the predicted mechanical response.
Crucially, the rubber modulus
Erubbery,eff(
χ) was coupled to the crystallinity
χ through a quadratic reinforcement factor in order to simulate the role of crystalline lamellae as physical cross-links in the amorphous matrix according to the equation:
where
represents the baseline modulus calculated according to the linear rule of mixtures, while
(here = 10) represents the reinforcement efficiency of the crystalline phase.
The quadratic dependency and the magnitude of the reinforcement efficiency (
= 10) are consistent with classical micromechanical frameworks for particle-reinforced elastomers and semi-crystalline polymers (such as the Guth–Gold or modified Halpin–Tsai formulations). In these theories, the higher-order structural coefficients typically fall within the range of 2 to 15, depending on the aspect ratio and structural anisotropy of the reinforcing domains—in this case, the crystalline lamellae. A value of
= 10 sits squarely within this theoretical boundary [
30,
31,
32]. In any case, to mitigate the impact of this assumption, a sensitivity analysis for the target property,
, is conducted in the upcoming
Section 3, evaluating scenarios where its nominal calculated value is both doubled and halved.
Despite the substantial Eglassy/Erubbery ratio (Eglassy ~ 109 Pa and Erubbery ~ 107 Pa), the χ-dependence of the glassy modulus is explicitly retained. While its influence is secondary compared to the orders-of-magnitude transitions in the rubbery regime, this approach ensures formal completeness and predictive accuracy across all structural transitions. A sensitivity analysis further validates the model stability and quantifies the impact of crystalline constraints on actuation dynamics.
To conclude, Young’s modulus
of the composite varies with temperature due to the glass-to-rubber transition of the polymer matrix and with the crystallinity grade
χ. The corresponding mathematical function that captures the polymer’s behavior, i.e., rigid below
Tg and softening above
Tg, is described by a sigmoidal function:
where Δ
Tts (here set to 1.35 °C) defines the width of the transition region, which governs the transition sharpness. The adoption of this expanded formulation is essential for the physical completeness of the model. While a simplified Young’s modulus formula provides a first approximation, it fails to account for the residual stress contributions and thermal expansion effects that are intrinsic to shape-memory polymers. Treating the stiffness as a global function
E(
T,
χ) ensures a seamless mathematical transition between the glassy and rubbery regimes. This ensures that the framework remains robust and predictive across the entire operational temperature range, providing a superior fit to experimental data compared to traditional uncoupled models.
For completeness, it is worth pointing out that the aforementioned transition width parameter ΔTts was set to 1.35 °C based on the mathematical properties of the sigmoidal formulation. In a logistic step function, the temperature span required to complete the bulk of the glass-to-rubber transition (from 10% to 90% of the modulus drop) is defined by ΔTspan = 2ln(9)·ΔTts ≃ 4.4·ΔTts. Substituting ΔTts = 1.35 °C yields an effective transition window of approximately 6 °C, which perfectly captures the sharp, narrow temperature range over which the experimental storage modulus of the PLA-based matrix undergoes its abrupt thermal softening. Furthermore, a sensitivity analysis is included in the results section, systematically assessing how uncertainty in this specific assumption propagates to the resulting macroscopic properties.
2.4.6. Thermo-Viscoelastic Model for Shape-Memory Bending in PLA/PCL Blends
The thermo-mechanical response of the PLA/PCL composite strip during the shape-memory cycle was modeled using a thermally activated viscoelastic bending formulation. Shape-memory polymers exhibit the ability to temporarily fix a mechanically imposed deformation and subsequently recover their original configuration upon thermal activation. This behavior arises from the temperature-dependent mobility of the polymer chains and the associated variation in the elastic modulus across the glass transition region. The deformation of the strip is characterized by the evolution of the bending angle
θ(
t), which represents the macroscopic curvature state of the specimen. During the programming stage, the sample is heated above its effective glass transition temperature
Tg,eff, where the material exhibits a rubbery-like behavior with relatively low stiffness and higher molecular mobility. Under these conditions, the bending angle increases progressively until a prescribed maximum deformation
θmax is reached. The imposed bending can be described as follows:
where
θ(
t) represents the instantaneous bending angle,
t is time, and
tb denotes the characteristic bending time required to reach the programmed deformation.
Following mechanical loading, the specimen is cooled below the effective glass transition temperature of the composite material. In this temperature regime, the mobility of polymer chains is strongly reduced, and the material transitions to a glassy state, while the effective elastic modulus increases significantly. As a consequence, the imposed deformation becomes temporarily frozen, and the bending angle should ideally remain constant during the fixation stage:
until the reheating stage begins at
t, i.e., the instant time
tr.
In reality, in contrast to ideal shape memory frameworks that assume a perfectly rigid fixation, the present model incorporates the elastic backspring and viscoelastic relaxation phenomena occurring immediately after the removal of the external constraint.
From a physical standpoint, Equation (13) is modified to describe the partial dissipation of the stored entropic energy that was not effectively ‘frozen’ during the cooling stage. This transition is governed by first-order relaxation kinetics, where the instantaneous bending angle
decays from the peak deformation
toward a stable fixation state
according to the following relationship:
where
is the final tightening angle (corresponding to
θmax·
Rf), while the parameter
denotes the instant of mechanical constraint removal. From a physical perspective, at this time instant, the external stress is nullified, and the polymer chains—no longer restricted by the macroscopic constraint—begin to undergo a spontaneous rearrangement driven by the entropic elasticity of the network, driven by the parameter
, which represents the characteristic relaxation time of the polymer network during the fixation stage. Physically, the latter quantifies the rate at which the macromolecular chains dissipate the residual elastic energy that was not effectively constrained by the glass transition.
Unlike constant-relaxation models, the present framework defines
as a state-dependent variable coupled to the instantaneous relative stiffness
/
for capturing the internal friction of the polymer chains on the basis of this equation:
where
represents the instantaneous elastic response time (baseline offset, equal to 0.5 s in the present study), and
is a viscoelastic coupling coefficient, assumed to be 2 here. Additionally, a sensitivity analysis is presented in the results section for this property to highlight the influence of the model calibration choice and its constituent variables.
This coupling captures the physics of the ‘freezing’ process: as the temperature drops and the elastic modulus increases toward the glassy plateau E(T, χ) → Eglassy,eff, the molecular mobility is progressively hindered by internal friction, leading to an increase in . From a rheological perspective, this dependency accounts for the time-temperature superposition principle within the fixation window. A higher signifies a more stable temporary shape, as the material requires more time to undergo further spontaneous deformation, thereby defining the kinetics of the elastic backspring and the ultimate precision of the shape-memory effect.
Upon reheating, the recovery process is governed by a thermally activated relaxation mechanism. Unlike ideal models that assume an instantaneous transition at
Tg, the present framework introduces a continuous activation function
α(
t) to account for the progressive mobilization of polymer chains within the glass transition region. Above this threshold, the molecular segments regain mobility, and the internal elastic energy stored during deformation drives the recovery toward the original configuration. This continuous activation function is modeled via a sigmoid activation function
according to the equation:
where
is a smoothing parameter defining the temperature breadth of the transition,
T(
t) is the instantaneous temperature of the sample, and
accounts for the thermal onset of the transition. This function ensures a continuous and physically consistent transition (avoiding numerical instabilities associated with ideal step functions) near the effective glass transition temperature
. According to this, the recovery is physically “frozen” (
α ≃ 0) in the glassy state and gradually “activated” (
α → 1) as the material reaches the transition region.
Furthermore, in the present model, the activation parameters are formulated as functions of the total crystallinity to capture its effect on the mobility of PLA/PCL blends. This coupling renders the shape-memory response both temperature-dependent and structurally sensitive, reflecting the role of the crystalline phase in modulating macromolecular flow. Specifically, higher crystallinity—typically associated with increased PCL content—results in a sharper and earlier activation of , thereby accelerating the relaxation kinetics.
In more detail, to account for the plasticizing effect induced by the PCL phase, the parameters
and
in Equation (16) are defined as linear functions with negative correlation to the total crystallinity of the blend:
where
and
represent the nominal activation offset and smoothing parameter, respectively, while
and
are sensitivity coefficients that quantify the plasticizing efficiency of the crystalline domains on the molecular mobility.
Then, the recovery kinetics can be modeled through a suitable and modified first-order viscoelastic relaxation law, which accounts for the progressive mobilization of polymer chains and the experimental evidence of an incomplete recovery process that is governed by the competition between thermal and internal resistive forces. To accurately capture the shape recovery kinetics of PLA/PCL blends, the evolution of the instantaneous recovery angle
θ(
t) is described by:
where
θperm =
θmax(1 −
Rr) is the residual bending angle that accounts for the permanent set due to irreversible chain sliding after the recovery process is complete. In other words, this term accounts for the constraints imposed by the crystalline phases (particularly PCL) or molecular entanglements that prevent a full return to the original configuration.
In order to capture the thermo-mechanical coupling of the shape-memory effect, and differently from other standard models, the above effective relaxation time
is assumed to dynamically scale with the instantaneous effective Young’s modulus
of the composite material, which varies significantly across the glass transition region, and the effective glassy modulus
. Furthermore, it is also explicitly coupled to the degree of crystallinity (
χ). The following relation is adopted:
where
τmin is the minimum response time (internal viscosity limit),
τrc is a reference relaxation constant defining the intrinsic recovery timescale of the material. Moreover, in this formulation,
λ is a semi-empirical constant representing the crystalline hindrance factor. The inclusion of
χ acknowledges that crystalline domains (from both PCL and, in particular, PLA phases) act as physical cross-links that increase the internal viscosity, thereby slowing down the recovery kinetics compared to an amorphous system.
Notably, the evolution of the bending angle is directly coupled with the thermal history and the intrinsic mechanical properties of the composite. This is achieved through the temperature-dependent elastic modulus,, which incorporates the contributions of both PLA and PCL phases via a rule-of-mixtures formulation, as previously described.
Integrating physical consistency with computational efficiency, this thermo-viscoelastic model captures the complexities of thermally activated shape-memory behavior. It enables precise simulation of the programming–fixation–recovery sequence, ensuring that internal viscosity is honored to avoid unphysical artifacts across diverse PLA/PCL ratios.
In the proposed mSLS framework, the activation/shape memory element
εs operates in series with the elastic spring E
1 within the upper branch. Its strain rate evolution
is governed by a thermally activated relaxation mechanism driven by the local elastic strain stored in the branch, scaled by the continuous activation function
and the effective relaxation time
, in agreement with the following equation:
where
is the total strain of the upper branch, while
is the strain associated with the stress relative to the spring
E1.
As expressed via Equation (16), the activation function couples temperature, stress-induced configurations, and blend crystallinity through the shifting of the effective glass transition temperature and the smoothing parameter .
When T(t) < Tg,eff, α → 0, which implies → 0, mathematically ensuring that the stored strain remains securely “frozen” in the glassy state.
Otherwise, when T(t) > Tg,eff, α → 1, activating the kinetic process where drives the system toward shape recovery.
2.4.7. Kinetic Analysis
As a theoretical foundation, the shape recovery process in polymeric shape-memory materials is inherently a time-dependent viscoelastic phenomenon, driven by the entropic restoration of macromolecular chains toward their equilibrium configuration. As illustrated in the following equation, the recovery of the residual strain
over time
t can be fundamentally approximated by an exponential decay law:
where
ε0 is the initial strain stored in the material after deformation. The physical driving force of this process is the instantaneous recovery rate, which defines the velocity of the entropic rebound. In our model, this instantaneous recovery rate (
Irr), defined as the magnitude of the angular variation over time
is characterized as the ratio between the current angular displacement from the equilibrium
, and the effective relaxation time
according to the relation:
By introducing the thermal activation factor
α(
T), the rate is dynamically modulated to account for the “thermomechanical switch” behavior occurring during the glass transition, where the internal viscosity drops, and molecular mobility is restored. Specifically, the evolution of the recovery angle
is computed into a discrete-time numerical framework, and at each time step, it is updated as follows:
To characterize the efficiency of the shape memory effect, a sensitivity analysis was performed by varying the bath temperature (Tbath) within the range of 45 °C to 75 °C. This allows for the identification of the peak recovery rate , which represents the maximum kinetic energy of the entropic rebound.
In the investigated limited temperature range, the non-linear Arrhenius dependence of the recovery kinetics can be accurately approximated by a first-order Taylor expansion. By defining
Tonset as the thermal threshold where the recovery process is initiated (i.e., the x-axis intercept where
= 0), the kinetic response simplifies to a linear relationship, of the form:
where
expressed in deg·s
−1·°C
−1 defines the thermal kinetic sensitivity, quantifying the acceleration of the deployment rate per unit increase in bath temperature.
This linear approximation neglects higher-order terms of the exponential expansion, providing a robust fit (R2 used as a reliability metric) within a ±15 °C window around the nominal temperature. Physically, according to the transient thermal model described by Newton’s Law of Cooling (Equation (10)), this linearity suggests that, in this temperature range, the heating rate is governed by the temperature gradient . Given the finite convective heat transfer coefficient (h = 200 W/m2K−1), the thermal relaxation time, acts as a physical filter that linearizes the response. In this condition, the peak recovery speed is dictated by the rate of energy inflow rather than the pure molecular mobility of the polymer chains. This linear dependency is of significant engineering interest, as it ensures highly predictable and controllable deployment velocities across the operational temperature range. Furthermore, the characteristic response time (Δtrec) is quantitatively defined as the time required to reach 63.2% of the total recoverable angle (θ63%), consistent with first-order kinetic conventions.
2.4.8. Stress–Strain Relationship
To provide a rigorous description of the blend’s mechanical behavior, the stress–strain relationship is modeled through a unified thermomechanical constitutive framework. This approach transcends simple linear elasticity by coupling the temperature-dependent stiffness with the internal strain states of the polymer network. The constitutive response is defined as follows to account for the interplay between mechanical, thermal, and inelastic strain components:
In the proposed framework, the value of the internal resistive force per unit area (σ) is subjected to a saturation limit (about 52 MPa) to account for the elasto-plastic transition and the frozen stress state reached after the thermoforming cycle.
The global effective Young’s modulus E(T, χ) in this context serves as the primary subject of the sensitivity analysis to evaluate how uncertainties in phase moduli (Ec and Ea) propagate to the macroscopic stress. In the above equation, εtot is the total applied strain. εth(T) represents the thermal strain, calculated as α·(Ttest − Tref) with a coefficient of thermal expansion α = 1.2 × 10−4 K−1 at the test temperature Ttest = 25 °C and a temperature of reference Tref = 0 °C. The selection of these thermal boundary conditions is substantiated by specific physical and experimental requirements. Ttest was fixed at 25 °C to reflect standard ambient laboratory conditions, ensuring that both the mechanical characterization and the subsequent shape recovery (springback) measurements were conducted under a controlled, reproducible environment. Concurrently, Tref was established at 0 °C to provide a robust athermal baseline, representing a theoretical stress-free state. This choice follows a well-established phenomenological convention in thermomechanical modeling, allowing for the precise quantification of the thermal offset, , accumulated as the material equilibrates from a reference state to the designated test temperature.
Finally, εin(T, χ) denotes the inelastic or “frozen” strain, which accounts for the internal stress state and structural constraints imposed by the crystalline lamellae. In the present treatment, this parameter was set to a constant value of 1.5 × 10−3 to represent the characteristic residual strain of the semi-crystalline system, thereby allowing a focused assessment of the stiffness-related parameters.
By explicitly incorporating ϵth and ϵin, the model accurately captures the effective driving force for mechanical response and the characteristic shift in the stress–strain origin. These specific values were selected based on preliminary experimental observations, which showed a consistent residual offset in the stress–strain origin for the PLA/PCL blends.
To further substantiate the robustness of this expanded framework, a comprehensive sensitivity analysis was performed on εth and εin. This assessment quantifies how fluctuations in these constitutive parameters—arising from experimental uncertainties or material variability—influence the overall thermomechanical response and the predicted shift in the stress–strain origin. By isolating the contribution of each term, we demonstrate the stability of the unified framework across a broad range of operational conditions.
2.4.9. Mechanical Modeling of Spatial Strain and Stress Distribution
To evaluate the thermomechanical robustness of the PLA/PCL blends, a localized elasto-plastic framework was developed to model the U-bending configuration (180° nominal angle), as illustrated by the experimental configuration of the previous
Figure 1. Unlike simplified linear models, this approach accounts for the severe plastic deformation (
ϵ ~ 16%) and the subsequent geometric recovery (springback) observed experimentally. The mechanical response of the analyzed 60 × 10 × 1 mm beam sample is modeled using a curvature approach at the bend apex. Under the Euler–Bernoulli assumption—where plane sections remain plane and perpendicular to the neutral axis—the curvature
(m
−1) is defined by the inner radius R
in and the half-thickness of the sample, rather than by the total sample length (
θ/
L), according to the equation:
To justify the choice of this framework under severe loading conditions, it is worth noting that a 180° U-bending with a 16% local strain implies a large deformation. However, for our bar geometry, the maximum local strain of 16% corresponds to an inner radius of
Rin = 2.625 mm. This yields a thickness-to-inner radius ratio (
Th/
Rin) of 0.38. Although this ratio places the beam section at the threshold of moderately thick structures during peak bending, the high global slenderness ratio (
L/
Th = 60) ensures that the Euler–Bernoulli hypothesis remains a sufficiently accurate and widely accepted approximation to predict the macroscopic mechanical behavior and subsequent shape recovery [
33].
For clarity, both strain and stress are herein regarded as spatiotemporal fields, formally expressed as
ε(
t,
y) and
σ(
t,
y), where
t denotes time and y is the through-thickness coordinate measured from the neutral axis. The present section focuses on their spatial distribution across the beam thickness at a given stage of the thermomechanical cycle, namely
ε(
y) and
σ(
y); conversely, their time-dependent constitutive evolution at a fixed material position,
ε(
t) and
σ(
t), is derived separately in the
Supplementary Information using the proposed rheological model.
Furthermore, under the assumption of uniform curvature along the beam, the solutions derived for the strain ε(t, y) during the loading, fixing, and unloading phases are directly mapped onto the macroscopic bending angle θ(t), preserving an identical temporal evolution.
The axial strain (
ε) varies linearly across the beam thickness (
y), ranging from maximum compression at the inner surface (
y = −
Th/2) to maximum tension at the outer surface (
y = +
Th/2). This distribution is governed by the following analytical equation:
It is important to point out that this linear kinematic relationship is maintained at the bend apex under the Euler–Bernoulli assumption for thin beams. While the global U-shape represents a large displacement regime, the local cross-sectional integrity is preserved, allowing the strain to be modeled as a linear function of the distance from the neutral axis, even as the constitutive response enters the non-linear regime during the thermo-mechanical vitrification process.
Regarding the evaluation of shape memory performance, the macroscopically measured angular recovery
θ(
t) was employed as a direct indicator of the local strain recovery. This kinematic correlation is justified by the fact that the maximum local flexural strain at the bend apex is uniquely defined by the localized curvature (κ), according to the plane-section assumption. Because the transformation-induced unloading and subsequent phase transformation during recovery lead to a homogeneous reduction in the apex curvature, a direct geometric proportionality exists between the springback/recovery of the subtended angle and the relaxation of the outer-fiber strain. Consequently, tracking the macroscopic angle remains a reliable and widely adopted proxy for evaluating the strain-level recovery in highly localized U-bending configurations [
34].
Given the high strain levels at the apex, the internal normal stress (
σ) deviates from the linear generalized Hooke’s law once the yield threshold of the blend is reached. The present study adopts a perfectly plastic constitutive model to capture the toughening effect of the PCL content, which enables stable plastic flow:
where
σy is the calibrated yield stress of the blend (
σy ~ 52 MPa). This saturation prevents unphysical stress predictions and accurately describes the formation of plastic hinges.
The bending moment (
M), representing the internal resistive couple resulting from the stress distribution, is calculated by integrating the stress over the cross-section area:
Upon release of the applied load, the elastic core of the sample (
σ <
) drives a partial geometric recovery. The springback factor
ks, representing the ratio between the final fixed angle (
θf) and the initial imposed maximum angle (
θmax = 180°), is determined by the residual moment capacity:
where
I = (
W·
Th3)/12 is the second moment of area for the rectangular cross-section. Finally, to quantify the blend’s ability to withstand severe deformation without fracture, the plastic dissipated energy density (
Udiss) is evaluated. The total work per unit volume is partitioned into recoverable elastic energy (
Uel) and dissipated plastic work:
This energetic mapping reveals that the PCL phase acts as a high-capacity energy sink at the outer fiber, effectively shielding the sample from brittle failure during the U-shape formation.