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Partial Equilibration Scenario in 3D athermal martensites
quenched below first-order transition temperatures

N. Shankaraiah1 , K.P.N. Murthy2 and S.R. Shenoy1 1Tata Institute of Fundamental Research-Hyderabad, Hyderabad, Telangana 500046, India.
2Dept of Physics, Central University of Rajasthan, Bandar Sindri, Rajasthan 305817, India
Abstract

To test a Partial Equilibration Scenario (PES) of Ritort and colleagues, we do Monte Carlo simulations of discretized-strain spin models, for four 3D martensitic structural transitions under quenches to a bath temperature T<T0T<T_{0} below a first-order transition. The ageing system faces entropy barriers, in searches for energy-lowering passages between quasi-microcanonical energy shells. We confirm the PES signature of an exponential-tail distribution of intermittent heat releases to the bath, scaled in an effective temperature, that in our case, depends on the quench. When its inverse βeff(T)1/Teff(T)\beta_{eff}(T)\equiv 1/T_{eff}(T) vanishes below a ‘martensite start’ temperature T1T_{1} of avalanche conversions, then entropy barriers vanish. When this search temperature Teff(T)T_{eff}(T) vanishes, PES cooling is arrested, as entropy barriers diverge. We find a linear vanishing of Teff(T)TdTT_{eff}(T)\sim T_{d}-T, below a delay-divergence temperature TdT_{d} in between, T1<Td<T0T_{1}<T_{d}<T_{0}. Martensitic conversion delays e1/Teffe1/(TdT)e^{1/T_{eff}}\sim e^{1/(T_{d}-T)} thus have Vogel-Fulcher-Tammann like divergences. Post-quench delay data extracted from simulations and athermal martensitic alloys, are both consistent with predictions.


I Introduction

The re-equilibration of a system after a quench is a long-standing problem in non-equilibrium statistical mechanics, and a generic Partial Equilibration Scenario (PES) has been proposed by Ritort and colleagues R1 ; R2 ; R3 ; R4 After a quench, the system spreads rapidly over an energy shell EE in configuration space. The system lowers its energy by intermittent energy releases δE<0\delta E<0 to the heat bath at TT, and then again spreads ergodically over the next energy shell E=E+δE<EE^{\prime}=E+\delta E<E. The iteration of the fast/ slow steps ratchets the system down to a canonical equilibrium at TT.The distribution of energy changes {δE}\{\delta E\} has a signature exponential tail R1 ; R2 ; R3 ; R4 in the heat release distribution P0(δE;tw)eδE/2Teff(tw)P_{0}(\delta E;t_{w})\sim e^{\delta E/2T_{eff}(t_{w})}, whose slope at the origin defines the (inverse) effective temperature βeff1/Teff\beta_{eff}\equiv 1/T_{eff}, dependent on the post-quench waiting time twt_{w}. The tail for negative energies is part of a shifted gaussian that peaks at positive energies. The PES has been confirmed through analytic Monte Carlo (MC) calculations of relaxing independent harmonic oscillators R1 ; R2 ; by simulations of spin-glass models and Lennard-Jones binary mixturesR3 ; R4 , and through voltage noise intermittency R3 . The MC updates of ageing harmonic oscillators R2 have to hit the ever-shrinking target of as yet unrelaxed oscillators, and these rising entropy barriers induce slow decreases in energies 1/lnt1/\ln t and acceptances 1/tlnt\sim 1/t\ln t.

It is natural to test PES ideas in interacting systems with slow relaxations. The structural glass transition R5 is an attempted equilibration that is arrested at a glassy freezing temperature TGT_{G}, pre-empting crystallization R5 ; R6 . The TT-dependent effective viscosity increases above a Vogel-Fulcher-Tammann (VFT) singularity R7 ; R8 e1/|TTG|e^{1/|T-T_{G}|}, that has been studied for a century, but is not yet fully understood. Further, decays around the glass temperature have non-exponential time dependence; and non-Debye frequency responses R9 . We consider other systems with structural transitions and equilibration delays. Martensitic steel alloys, when quenched from high temperature parent austenite to low temperature ‘martensite’ R10 ; R11 , show strain domain-wallR12 patterns R13 ; R14 ; R15 .They can exhibit puzzling delays in conversion to martensite R16 ; R17 ; R18 ; R19 ; R20 , that increase rapidly with temperature: raising TT to nearer transition by a few percent, can raise delays from 11 sec to 10410^{4} seconds R18 .

We do Monte Carlo (MC) simulations of quenches in TT, of martensitic discretized-strainR21 ; R22 ; R23 models in 3D. The model hamiltonians describe the elastic Domain Walls (DW) or mobile twin boundaries, of four 3D structural transitions, each with characteristic anisotropic Compatibility interactions between order-parameter strainsR15 . The four transitions R21 can occur in martensite-related functional materials, where OP strains will be coupled to the functionality variables. The transitions are tetragonal-orthorhombic (YBCO, superconductivity); cubic-tetragonal (FePd, shape memory); cubic-orthorhombic (BaTiO, ferroelectrics); cubic trigonal (LaSrMnO, colossal magnetoresistance).

Our 3D simulations yield post-quench evolutions as in R24 ; R25 ; R26 2D, passing through three Domain Wall (DW) states. At first there is a majority-austenite DW Vapour state of a martensite droplet in an austenite background. This converts to majority-martensite DW Liquid, of randomly wandering walls. Finally the DW Liquid orders to a DW Crystal microstructure, with the walls along preferred directions R13 , as in parallel ‘twins’.

We focus on the conversion delays of the first evolution of DW Vapour \rightarrow DW Liquid, that corresponds to austenite to martensite conversions, or a rise of the martensite fraction nm(t)n_{m}(t) from zero to unity. As in the earlier 2D case R24 ; R25 ; R26 , a phase diagram in material parameters is obtained. In the ‘athermal’ martensite regime, there are curious ‘incubations’, or no apparent changes after a quench, terminated by sudden avalanche conversions R16 ; R17 ; R18 ; R19 ; R20 . In this regime, we find three characteristic temperatures, with T1<Td<T0T_{1}<T_{d}<T_{0}. Here T0T_{0} is the meanfield transition to uniform ordering.

Avalanche conversions in a single MC time step tm=1t_{m}=1,occur for T<T1T<T_{1}, identified as the martensite start temperatureR10 ; R11 Ms=T1M_{s}=T_{1}. Quenches into T1<T<TdT_{1}<T<T_{d} show (postponed) avalanches R27 or incubation behaviour: the conversion fraction nm(t)n_{m}(t) remains flat at zero, until there is a jump up to unity a time t=tm(T)t=t_{m}(T). The incubation delay time tm(T)t_{m}(T) extends rapidly, on approaching a divergence temperature TdT_{d}.The physical picture for delays is of Vapour-droplet Fourier profile attempting entry to a negative-energy region of effective Hamiltonian spectra ϵ(k,T)<0\epsilon(\vec{k},T)<0. The profile has to pass through a zero-energy k\vec{k}-space contour at a bottleneck, like a Golf Hole edge R28 ; R29 ; R30 ; R31 . This transit passage delay differs from the familiar critical slowing down from a divergent Order Parameter length. The TT-dependent, anisotropic bottleneck shrinks on warming, with a topological shape change at TdT_{d}, that blocks entry, so entropy barriers diverge. The precursorR14 ; R15 region Td<T<T0T_{d}<T<T_{0}, where 2D results suggest dynamic tweed R27 , may be studied elsewhere.

We use generic equilibration scenario of Ritort and colleagues to analyze the statistics R1 ; R2 ; R3 ; R4 ; R31 , of the set of energy changes {δE}\{\delta E\} from each MC step (usually used but not retained R32 ). These heat releases are recorded only up to an aging time tw=tm(T)t_{w}=t_{m}(T), so the effective temperature depends on the quench temperature, Teff(tw)Teff(T)T_{eff}(t_{w})\rightarrow T_{eff}(T): non-stationary distributions become time independent. We confirm the signature PES exponential tail for all four transitions. We find the search temperature vanishes linearly Teff(T)TdTT_{eff}(T)\sim T_{d}-T, driving an entropy barrier divergence at TdT_{d}. The martensite-conversion times are thus predicted to show glass-like VFT behaviour, e1/Teff(T)e1/(TdT)\ e^{1/T_{eff}(T)}\sim e^{1/(T_{d}-T)} here understood as an arrest of PES cooling. Such VFT behaviour, is extracted from simulation and experimental R16 ; R17 ; R18 data.

Refer to caption
Figure 1: Schematic of Partial Equilibration Scenario : The system in a configurational shell of states with energy EE, states Ω(E)\Omega(E), and entropy S(E)=lnΩ(E)S(E)=\ln\Omega(E) makes a passage to the next shell of lower E<EE^{\prime}<E, fewer states Ω(E)<Ω(E)\Omega(E^{\prime})<\Omega(E) and smaller entropy S(E)<S(E)S(E^{\prime})<S(E), crossing a generic entropy barrier to find rarer states. The turned-back wiggly lines are failed searches for passage. The downward bold line denotes successful searches, accompanied by a distribution of heat releases δEEE<0\delta E\equiv E^{\prime}-E<0 to the bath at TT, scaled in an effective search temperature TeffT_{eff}. Our case of quenches below a first-order transition can have further, specific entropy barriers, eg hindering system passage through order parameter-related, TT-dependent, bottlenecks in phase-space.

The plan of the paper is as follows. In Section II, we discuss the generic Partial Equilibration Scenario and our specific case of quenching across a phase transition. Section III describes for the four transitions in 3D, the discrete-strain clock-like spins and their TT-dependent Hamiltonians. In Section IV we describe the MC simulations, with delay results from the phase space bottlenecks in Section V. Section VI shows that PES signatures are seen in all four transitions. Section VII shows that both 3D simulations and metallic alloy experiments exhibit VFT behaviour. Finally Section VIII is a summary.

Appendix A illustrates how a continuum double-well Landau free energy induces a T-dependent, Ising effective Hamiltonian. Appendix B obtains the athermal phase diagram for four transitions. Movies of post-quench DW evolutions are in Supplementary Material Videos R27 .

Refer to caption
Figure 2: Microstructures in ferroelastic transition: The Domain Wall crystal or twinned textures are shown, with variant label VV in the colour bar. The Hamiltonian energy scale in is E0=3E_{0}=3, with the non-OP compressional constant A1=4A_{1}=4 fixing all other non-OP elastic constants, see text. The DW textures are (a) tetragonal-orthorhombic transition at T=0.45T=0.45 and Landau spinodal temperature Tc=0.95T_{c}=0.95; (b) cubic-tetragonal transition at T=0.4T=0.4 and Tc=0.95T_{c}=0.95; (c) cubic-orthorhombic transition at T=0.3T=0.3 and Tc=0.95T_{c}=0.95; and (d) cubic-trigonal transition at T=0.37T=0.37 and Tc=0.97T_{c}=0.97. Note that for each transition, all allowed variants are actually present.

II Scenario for post-quench equilibration:

How do systems re-equilibrate, after a temperature quench? Ritort and coworkers have suggested that if an equilibrium canonical ensemble in thermal contact with a heat bath suddenly has its bath quenched to a lower temperature TT, then the system goes into an ageing ensembleR1 ; R2 ; R3 ; R4 , that has a quasi- microcanonical description of states of the system. There are sequential passages through decreasing-energy configurational shells, and intervening entropy barriers in the system-search for the new equilibrium. While delays from energy barriers are from attempts through activated jumps, to cross mountains, delays from entropy barriers are from attempts through constant-energy searches, to find rare channels going through or around, the mountain R31 .

In this Section we i) outline (our understanding of) the generic Partial Equilibration Ensemble R1 ; R2 ; R3 ; R4 or PES, and ii) state how this ageing scenario is applied to our specific case, that has quenches across phase transitions, and order parameter emergence from zero.

i) Generic PES for ageing after quenches:

The PES for the equilibration process considers a system of energy EE in contact with a (larger) heat bath. A familiar textbook derivation R33 of the canonical ensemble, applies the microcanonical ensemble to the system plus heat bath, of constant total energy Etot=E+EbathE_{tot}=E+E_{bath}. The total number of states is the product of the Ω(E)\Omega(E) states of the system, and of the Ωbath(EtotE)\Omega_{bath}(E_{tot}-E) states of the bath, summed over all allowed system energies 0<E<Etot0<E<E_{tot}:

Ωtot(Etot)=EΩ(E)Ωbath(EtotE).\Omega_{tot}(E_{tot})=\sum_{E}\Omega(E)\Omega_{bath}(E_{tot}-E). (1)

The system configurational entropy is S(E)=lnΩ(E)S(E)=\ln\Omega(E), and the inverse effective temperature is βeff1/Teff=dS(E)/dE\beta_{eff}\equiv 1/T_{eff}=dS(E)/dE. Similarly, the inverse bath temperature is βbath1/Tbath=dSbath/dEbath\beta_{bath}\equiv 1/T_{bath}=dS_{bath}/dE_{bath}. The change in total entropy depends on the system energy change dEdE as

dStot=dS(E)dEdE+dSbathdEbathdEbath=[βeffβbath]dE0dS_{tot}=\frac{dS(E)}{dE}dE+\frac{dS_{bath}}{dE_{bath}}dE_{bath}=[\beta_{eff}-\beta_{bath}]dE\geq 0 (2)

with the equality at equilibrium, when the system and bath temperatures are equal βeff=βbath\beta_{eff}=\beta_{bath}. The Second Law inequality dStot>0dS_{tot}>0 must hold, for the irreversible cases. After a bath quench from initial to a final Tbath=TT_{bath}=T, the system is left hotter, Teff>TT_{eff}>T, or βeffβ<0\beta_{eff}-\beta<0. The energy changes are negative dE=dQ<0dE=dQ<0, with heat released by the system to the bath.

At equilibrium, the terms in the sum of Equ (1) are dominated by clusters of energy shells selected R33 by a sharp peak, arising from the product of a rising number of system states Ω(E)\Omega(E), and a falling bath factor eE/Tbathe^{-E/T_{bath}}. The peak width is the energy fluctuations from stochastic system-bath exchanges. These equilibrium ideas describe states, not processes.

The Partial Equilibration Scenario postulates a plausible post-quench non-equilibrium process for the system to evolve between the initial and the final equilibrium state. A sudden change in bath temperature or quench, will induce a shifted peak, around a different equilibrium state. The post-quench system, initially stranded in non-optimum states, is visualized as moving through the sequentially lower energy shells of Equ (1) in its search for the shifted peak, tracked by an ageing time twt_{w}.

The Scenario postulates that the system i) rapidly spreads ergodically through all states of a shell of energy E, and ii) slowly dribbles out energy {δE}\{\delta E\} to the ever-present energy bath. Since the system is partially equilibrated in the quasi-microcanonical shell, the equilibrium definitions can be retained, of the shell entropy S(E)S(E) and its energy derivative 1/Teff(tw)1/T_{eff}(t_{w}). The back-and-forth energy exchanges to rapidly surmount internal energy barriers and explore all shell configurations, are summoned by the system from the bath (‘stimulated’). The slow changes on passages to a lower-energy shell, are releases by the system to the bath (’spontaneous’).

Fig 1 is a schematic of the Partial Equilibration Scenario. The successive shells have lower energy E<EE^{\prime}<E and hence lower number of configurations Ω(E)<Ω(E)\Omega(E^{\prime})<\Omega(E) and entropies S(E)<S(E)S(E^{\prime})<S(E). There is a generic entropy barrier SBΔS=ln[Ω(E)/Ω(E)]>0S_{B}\equiv-\Delta S=-\ln[\Omega(E^{\prime})/\Omega(E)]>0 to finding the rarer states. Key seeks lock: most attempts fail.

From an ageing Fluctuation Relation R3 the nonequilibrium energy-change probability R1 ; R2 ; R3 ; R4 is a peak at the origin, times an exponential tail for negative changes. This generic PES signature tail depends on the ageing time through the the effective temperature Teff(tw)T_{eff}(t_{w}), that scales the heat releases:

P0(δE;tw)P(+)0(δE;tw)eδE/2Teff(tw),P_{0}(\delta E;t_{w})\simeq{P^{(+)}}_{0}(\delta E;t_{w})e^{\delta E/2T_{eff}(t_{w})}, (3)

with an even prefactor P(+)0(δE;tw){P^{(+)}}_{0}(\delta E;t_{w}).

In an important result, other effective temperatures, from the Fluctuation-Dissipation Theorem; and from non-equilibrium fluctuations of system variables, are shown to be equal to the PES effective temperature R1 : there is only one TeffT_{eff}.

Refer to caption
Figure 3: Conversion incubations ending in postponed avalanches: Four-panel plot of martensite conversion fraction nm(t)n_{m}(t) versus time tt, for fixed E0=3E_{0}=3, A1=4A_{1}=4 and different scaled temperatures |δ0(T)||TTd|/Td|\delta_{0}(T)|\equiv|T-T_{d}|/T_{d} as in the legend. There are flat incubations ending in explosive jumps in nm(t)n_{m}(t) at t=tmt=t_{m} defined by nm(tm)=1/2n_{m}(t_{m})=1/2. (a) tetragonal-orthorhombic transition with Landau spinodal temperature Tc=0.9T_{c}=0.9; (b) cubic-tetragonal transition with Tc=0.95T_{c}=0.95; (c) cubic-orthorhombic transition with Tc=0.95T_{c}=0.95; (d) cubic-trigonal transition with Tc=0.97T_{c}=0.97, that is unusual, see text.
Refer to caption
Figure 4: Acceptance spikes and energy drops: Four-panel plots for all transitions, showing Acceptance fractions Aacc(t)A_{acc}(t) and total energies E(t)E(t) versus time (displaced above and below the xx-axis, for clarity). For T<T1T<T_{1}, eg for δ0=0.7\delta_{0}=-0.7, there are immediate spikes in Aacc(t)A_{acc}(t), and drops to negative values in energy E(t)E(t), at the very first MC sweep t=1t=1 as denoted by on-axis blue solid circles. For T>T1T>T_{1} eg for δ0=0.1\delta_{0}=-0.1, the red open squares show there are flat lines of incubation ending at t=tmt=t_{m} postponed spikes and drops. The transitions a), b), c), d) are as in the Fig 3 Caption. Again, the cubic-trigonal case d) is unusual.

ii) Specific PES from quenching across a transition.

For our case of quenching to TT across a first-order transition, the Order Parameter (OP) has to rise from zero, and so the wait times twt_{w} to reach OP marker events will depend on the quench temperature, tw=tm(T)t_{w}=t_{m}(T).The effective temperature and PES distribution will thus also depend on the quench temperature, Teff(tw)Teff(T)T_{eff}(t_{w})\rightarrow T_{eff}(T) and P0(δE;tw)P0(δE,T)P_{0}(\delta E;t_{w})\rightarrow P_{0}(\delta E,T). The even prefactor P0(+)(δE,T)P^{(+)}_{0}(\delta E,T) can be exponentiated and expanded to quadratic order, Equ (3) is then a gaussian peaked at the origin, times an exponential falloff. Completing the square yields a PES signature of a shifted gaussian, peaked at positive mean changes M(T)=<δE>M(T)=<\delta E>, and scaled in TeffT_{eff}:

P0(δE,T)e[δEM(T)]2/4M(T)Teff(T).P_{0}(\delta E,T)\simeq e^{-[\delta E-M(T)]^{2}/4M(T)T_{eff}(T)}. (4)

For small heat releases δE=|δE|<0\delta E=-|\delta E|<0, the PES distribution takes a Boltzmann-like form P0e12βeff(T)|δE|P_{0}\simeq e^{-\frac{1}{2}\beta_{eff}(T)|\delta E|}. This gives a physical meaning to the effective temperature: it is a search range for accessible energy shells. If βeff0\beta_{eff}\rightarrow 0, entropy barriers collapse, and passages are immediate. If Teff0T_{eff}\rightarrow 0, then entropy barriers diverge, and passage-searches freeze.

We postulate that the OP-related bottlenecks can be of two types, depending on the depth of the quench. a) The DW Vapour \rightarrow Liquid delays are attributed to phase space bottlenecks R27 , suggested by concepts in protein folding R28 ; R29 ; R30 . Hamiltonian energy-spectrum contours in Fourier space of zero energy are like a TT-dependent Golf Hole (GH) edge, with a negative-energy Funnel region inside it leading to the final state R28 . The entropic delays are from finding and entering the bottleneck.
b) For deeper quenches, the DW Liquid \rightarrow Crystal delays could be conceptually related to spin facilitation models R27 ; R34 ; R35 , through the TT-dependent sparseness of austenitic-hotspot dynamical catalysts, or other facilitating fields R20 ; R27 .

III Domain-wall Hamiltonians for four structural transitions in 3D:

The transition-specific, derived effective Hamiltonians have been presented in detailR15 ; R21 ; R22 ; R23 ; R24 ; R25 ; R26 , and we just outline as conceptual background: A) Strains and Compatibility constraints. B) Reduction of continuum strains to discrete-strain ‘pseudo-spins’. C) Reduction of continuum strain free energies to effective ‘spin’ Hamiltonians.

It is useful to define NOPN_{OP} the number of components of the OP strains; and NVN_{V} the number of Landau ‘variant’ minima at nonzero OP strain values. In terms of discretized strains, NOPN_{OP} is the number of vector spin components, that can point in NVN_{V} variant directions. A double-well Landau free energy for a scalar magnetization maps onto (Appendix A) an Ising model with NOP=1N_{OP}=1 and NV=2N_{V}=2. We consider four first-order transitions R21 with NOP=1,2,2,3N_{OP}=1,2,2,3. The nonzero, unit-magnitude variant vectors point respectively to corners of symmetry-dictated polyhedra with NV=2,3,6,4N_{V}=2,3,6,4 corners, inscribed in a unit circle or unit sphere: a geometrically pleasing sequence of line, triangle, hexagon, and tetrahedron. These transitions are respectively, tetragonal-orthorhombic, cubic-tetragonal, cubic-orthorhombic, and cubic-trigonal.

III.1 Strains and Compatibility:

Strains are symmetric tensors 𝐞=𝐞T{\bf e}={\bf e}^{T}, where the superscript TT is Transpose. In three spatial dimensions, there are 6 independent Cartesian strains R21 ; R23 exx,eyy,ezz,exy,eyz,ezxe_{xx},e_{yy},e_{zz},e_{xy},e_{yz},e_{zx}. The physical strains e1,e2e6e_{1},e_{2}...e_{6} are convenient linear combinations: one compressional e1=(exx+eyy+ezz)/6e_{1}=(e_{xx}+e_{yy}+e_{zz})/\sqrt{6}; two deviatoric or rectangular e2=(exxeyy)/2,e3=(2ezzexxeyy)/6e_{2}=(e_{xx}-e_{yy})/\sqrt{2},~{}e_{3}=(2e_{zz}-e_{xx}-e_{yy})/\sqrt{6}, and three shears e4=eyz,e5=ezx,e6=exye_{4}=e_{yz},e_{5}=e_{zx},e_{6}=e_{xy}.

The free energy R21 has a nonlinear Landau term that depends on a subset NOPN_{OP} of these physical strains, as the Order Parameter(s). The remaining n=6NOPn=6-N_{OP} non-Order Parameter physical strains enter the free energy as harmonic springs, whose extensions cannot be simply be set equal to zero, as pointed out by Kartha R15 . This is because a local OP-strained unit cell will generate non-OP strains in surrounding unit cells. To maintain lattice integrity all strained unit cells must mutually adapt, to all fit together in a smoothly compatible way, without dislocations.

For electromagnetism, there is a no-monopole Maxwell condition of vanishing divergence of the magnetic induction vector, .B=0\nabla.{\vec{B}}=0. For elasticity, there is a no-dislocation St Venant Compatibility condition of a vanishing double curl R15 , of the Cartesian strain tensor. In coordinate and Fourier space,

×[×𝐞(r)]T=0;K(k)×𝐞(k)×K(k)=0.\nabla\times[\nabla\times{\bf e}(\vec{r})]^{T}=\vec{0};\\ ~{}~{}{\vec{K}}(\vec{k})\times{\bf e}(\vec{k})\times{\vec{K}}(\vec{k})=\vec{0}. (5)

Here Kμ(k)2sin(kμa0/2)K_{\mu}(\vec{k})\equiv 2\sin(k_{\mu}a_{0}/2) for μ=x,y,z\mu=x,y,z, and lattice constant a0=1a_{0}=1. There are six differential-equation constraints, that are algebraic equations in Fourier space, of which only three are independent R21 ; R23 . Going to physical strains e1,e2e6e_{1},e_{2}...e_{6} the three k0\vec{k}\neq 0 algebraic equations express the non-OP strains in terms of the OP strains. The uniform k=0\vec{k}=0 non-OP strains are not so constrained, and can be freely set to their minimum value of zero.

The harmonic non-OP terms can then be analytically minimized subject to the k0\vec{k}\neq 0 linear constraints, by direct substitution for non-OP strains or by Lagrange multipliers. This yields an OP-OP effective interaction, with a transition-specific Compatibility Fourier kernel R15 that depends on direction k^k/|k|\hat{k}\equiv\vec{k}/|\vec{k}|. The kernels all have a prefactor νk1δk,0\nu_{\vec{k}}\equiv 1-\delta_{\vec{k},\vec{0}}, that vanishes for k=0\vec{k}=\vec{0}. The Compatibility kernels are smallest (eg zero) for specific directions k^\hat{k}, explaining the observed DW orientation along preferred crystallographic directions. The Compatibility potential in coordinate space is an anisotropic powerlaw, with the spatial dimensionality d=3d=3 as the fall-off exponent 1/Rd\sim 1/R^{d}.

Refer to caption
Figure 5: Conversion-success fraction: The successfully converting fraction Φm(T)\Phi_{m}(T) over 100 runs versus δ0(T)(TTd)/Td\delta_{0}(T)\equiv(T-T_{d})/T_{d} is shown in the range T1<T<T0T_{1}<T<T_{0}. The colours of symbols top to bottom denote transitions in order a) tetragonal-orthorhombic, b) cubic-tetragonal, c) cubic-orthorhombic, and d) cubic-trigonal. For a ‘precursor’ region T0>T>TdT_{0}>T>T_{d}, conversions do not occur. Success fractions are not exponentially sensitive to Hamiltonian energy scales E0=3,4,5,6E_{0}=3,4,5,6, and are hence attributed to entropy barriers.

III.2 Discrete-strain pseudo-spins:

Refer to caption
Figure 6: Delay times versus quench temperature: Linear-linear plots of mean conversion delay time t¯m{\bar{t}}_{m} versus scaled temperature δ0(T)(TTd)/Td\delta_{0}(T)\equiv(T-T_{d})/T_{d} for E0=3E_{0}=3, and various A1A_{1} elastic constants for the four transitions. (The symbol colours top to bottom denote transitions in the same order as Fig 5.) On approaching TdT_{d}, there are increasing standard-deviation error bars, suggesting a broadening rate distribution.
Refer to caption
Figure 7: Distribution of conversion rates: Four-panel plot of conversion rate distributions P(rm)P(r_{m}) versus rate rmr_{m} for E0=3,A1=4E_{0}=3,A_{1}=4 and different |δ0(T)||\delta_{0}(T)| as in the legend. Log-normal distributions are shown as guides to the eye. Transitions are again in the order a) tetragonal-orthorhombic transition; b) cubic-tetragonal transition; c) cubic-orthorhombic transition; and d) cubic-trigonal transition. Fast processes are narrow, while slow processes are broad.

The Landau free energy functionals fL(e)f_{L}(\vec{e}) for a first order transition can be scaled to be independent or weakly dependent, on material parameters R21 . With NOPN_{OP} physical strains as a vector e\vec{e} in OP space, the Landau free energy fL(e)f_{L}(\vec{e}) in the austenite phase always has a turning point at e=0\vec{e}=\vec{0}. In the martensite phase, it additionally develops NVN_{V} variant minima at e0\vec{e}\neq 0.

For first-order transitions, the scaled temperature is R21 ; R22 ; R23 ; R24 ; R25 ; R26 ,

τ(T)(TTc)/(T0Tc).\tau(T)\equiv(T-T_{c})/(T_{0}-T_{c}). (6)

All energies are scaled in the thermodynamic Landau temperature where austenite and martensite free energies cross, so the scaled T0=1T_{0}=1. Here Tc<T0T_{c}<T_{0} is the spinodal temperature where the austenite minimum vanishes, so uniform bulk austenite becomes unstable for T<TcT<T_{c}.

The local vector OP can be written as a product of magnitude and direction e(r)=|e(r)|S(r)\vec{e}(\vec{r})=|\vec{e}(\vec{r})|{\vec{S}}(\vec{r}). The NVN_{V} directions of variant or ‘spin’ vectors S(r){\vec{S}}(\vec{r}) identify the degenerate variants on either side of a Domain Wall (DW), with all having unit magnitude, S(r)2=S(r)2=1\vec{S}(\vec{r})^{2}=\sum_{\ell}S_{\ell}(\vec{r})^{2}=1. Since austenite is always a Landau turning point, and in any case austenite could be induced at any TT by local stresses, we always also include the austenite origin point S(r)=0\vec{S}(\vec{r})=\vec{0} as an allowed value R21 ; R22 ; R24 .

The strain magnitudes are flat, deep into domains on either side of narrow Domain Walls that are zeros of the OP. The local strain magnitude is set equal to the uniform Landau mean value R21 , |e(r)|ε¯(T)>0|\vec{e}(\vec{r})|\simeq{\bar{\varepsilon}}(T)>0, so components =1,2..NV\ell=1,2..N_{V} are approximated as

e(r)ε¯(T)S(r).e_{\ell}(\vec{r})\rightarrow{\bar{\varepsilon}}(T)S_{\ell}(\vec{r}).~{}~{} (7)

Substituting into the variational free energy density R21 with Landau,Ginzburg, and Compatibility terms f=fL(e)+fG(e)+fC(e)f=f_{L}(\vec{e})+f_{G}(\nabla\vec{e})+f_{C}(\vec{e}), generates a TT-dependent effective spin Hamiltonian H(S,T)H(\vec{S},T), with the same three terms, inheriting material-specific parameters such as Tc,T0,A1T_{c},T_{0},A_{1}. Each of the discretized-strain clock-like Hamiltonians have been systematically derived R21 from continuous-strain free energies. They are bilinear in the spins, and encode the crystal symmetries, strain nonlinearities, and Compatibility constraints.

The DW Hamiltonian, with E0E_{0} an energy scale (in units of T0T_{0}), is

F=E0r[fL+fG+fC]H(S,T)=HL(S,T)+HG(S)+HC(S).\begin{array}[]{rr}\displaystyle{F=E_{0}\sum_{\vec{r}}[f_{L}+f_{G}+f_{C}]}\\ \displaystyle{\rightarrow H(\vec{S},T)=H_{L}(\vec{S},T)+H_{G}(\nabla\vec{S})+H_{C}(\vec{S}).}\end{array} (8)

Notice HH has an inherent separation of time scales, with the magnitude ε¯(T){\bar{\varepsilon}}(T) responding immediately to quenches T<T0T<T_{0} in a single time-step, while the more sluggish DW adjustments of S(r)\vec{S}(\vec{r}) can take hundreds or thousands of MC time-steps.

With S6=S4=S2=0,1\vec{S}^{6}=\vec{S}^{4}=\vec{S}^{2}=0,1, the Landau term is

rfL(e)rfL(ε¯S)=fL(T)rS(r)2.\sum_{\vec{r}}f_{L}(\vec{e})\rightarrow\sum_{\vec{r}}f_{L}({\bar{\varepsilon}}\vec{S})=f_{L}(T)\sum_{\vec{r}}{\vec{S}}(\vec{r})^{2}.~{}~{}~{} (9)

The Landau free energy density is

fL(T)ε¯(τ)2gL(T)0,f_{L}(T)\equiv{{\bar{\varepsilon}}(\tau)}^{2}g_{L}(T)\leq 0, (10)

defining a factor gL(T)g_{L}(T), that vanishes at the Landau transition temperature gL(T0)=0g_{L}(T_{0})=0, and is negative below it.

For a uniform variant S(r)=S0\vec{S}(\vec{r})=\vec{S}_{0} a constant vector, or in Fourier space S(k)δk,0S0\vec{S}(\vec{k})\sim\delta_{\vec{k},0}\vec{S}_{0}, there is a vanishing of the Ginzburg term k2\sim{\vec{k}}^{2}, and of the Compatibility kernel νk=1δk,0\sim\nu_{\vec{k}}=1-\delta_{\vec{k},0}. The uniform (Landau) free energy then sets a lower bound to the energy, H(S,T)Nnm(t)fL(T)<0H(\vec{S},T)\geq Nn_{m}(t)f_{L}(T)<0, where the martensite fraction is

nm(t)(1/N)rS(r,t)2.n_{m}(t)\equiv(1/N)\sum_{\vec{r}}{\vec{S}(\vec{r},t)}^{2}. (11)

so nm=1n_{m}=1 or 0 for uniform martensite or austenite.

As a 2D illustration R24 ; R25 ; R26 , the square-rectangle OP is a scalar, so NOP=1N_{OP}=1. There are two variants (rectangles along either xx or yy axes), so NV=2N_{V}=2. The Landau free energy fL=e2[(τ1)+(e21)2]f_{L}=e^{2}[(\tau-1)+(e^{2}-1)^{2}] is a triple well in the OP strains. For τ=1\tau=1, the three well depths at e=0,±1e=0,\pm 1 are degenerate at zero. For 0<τ<10<\tau<1 the austenite well at e=0e=0 is metastable, and goes unstable at τ=0\tau=0, the T=TcT=T_{c} spinodal temperature. The Hamiltonian is diagonal in k\vec{k} space, βH=(D0/2)k[ϵ(k,T)|S(k)|2]\beta H=(D_{0}/2)\sum_{\vec{k}}[\epsilon(\vec{k},T)|S(\vec{k})|^{2}], where D0(2ε¯2E0/T)D_{0}\equiv(2{\bar{\varepsilon}}^{2}E_{0}/T). The energy spectrum for long wavelengths is ϵ(k,T)=[|gL(T)|+ξ02k2+A1U(k^)]\epsilon(\vec{k},T)=[-|g_{L}(T)|+{\xi_{0}}^{2}k^{2}+A_{1}U(\hat{k})]. The square-rectangle transition kernel depends on direction k^=k/|k|\hat{k}={\vec{k}}/|\vec{k}|, or the single polar angle ϕ\phi, as

U(k)=νk(k^x2k^y2)2[1+(8A1/A3)k^x2k^y2]=νk(cos2ϕ)2[1+(2A1/A3)(sin2ϕ)2]U(\vec{k})=\frac{\nu_{\vec{k}}({\hat{k}}_{x}^{2}-{\hat{k}}_{y}^{2})^{2}}{[1+(8A_{1}/A_{3}){\hat{k}}_{x}^{2}{\hat{k}}_{y}^{2}]}=\frac{\nu_{\vec{k}}(\cos 2\phi)^{2}}{[1+(2A_{1}/A_{3})(\sin 2\phi)^{2}]} (12)

where A3/A1A_{3}/A_{1} is the ratio of a non-OP (shear) elastic constant, and the non-OP compressional A1A_{1}. The (positive) kernel has a maximum value U(max)=1U(max)=1 at ϕ=±π/2\phi=\pm\pi/2, and a minimum value U(min)=0U(min)=0 at ϕ=±π/4\phi=\pm\pi/4, driving a preferred DW orientation along both diagonals.

The energy spectrum for A1=0A_{1}=0 is a parabola pulled down to negative values by the Landau term, ϵ[k2|gL(T)|]\epsilon\sim[k^{2}-|g_{L}(T)|]. A zero energy contour in (kx,ky)(k_{x},k_{y}) space is a circle with a T-dependent radius |gL(T)|\sqrt{|g_{L}(T)|}, that shrinks to a point at T0T_{0}. For A10A_{1}\neq 0, the bottleneck becomes angularly modulated, with a squared-radius k2(T,ϕ)=|gL(T)|(A1/2)U(k^)k^{2}(T,\phi)=|g_{L}(T)|-(A_{1}/2)U(\hat{k}), interpolating between a ϕ=±π/4\phi=\pm\pi/4 outer radius kouter2(T)=|gL(T)|k^{2}_{outer}(T)=|g_{L}(T)| and a ϕ=±π/2\phi=\pm\pi/2 inner radius kinner2(T)=|gL(T)|(A1/2)k^{2}_{inner}(T)=|g_{L}(T)|-(A_{1}/2). The inner radius clearly vanishes at some temperature |gL(Td)|=(A1/2)|g_{L}(T_{d})|=(A_{1}/2) where Td<T0T_{d}<T_{0}. This characteristic temperature, from an interplay between Landau, Ginzburg, and Compatibility terms, is where the entropy barrier diverges.

Planes et al R36 consider a uniform-martensite model with a Landau variational term fL(e,T)f_{L}(e,T). Fast or slow behaviour is through first-passage-time jumps crossing an energy barrier, that collapses at TcT_{c}, or is largest at T0T_{0}. Our spatially non-uniform martensite model with Ginzburg, Compatibility and Landau variational terms, differs in detail, but is similar in spirit. Fast or slow behaviour is through MC searches crossing an entropy barrier, that collapses at T1T_{1} and diverges at TdT_{d}.

III.3 DW Hamiltonians for four transitions :

Clock models have discrete spins directed at NVN_{V} points on a unit circle, and are denoted by NV\mathbb{Z}_{N_{V}}, where the Ising model is 2\mathbb{Z}_{2}. Here we generalize to include S=0\vec{S}=\vec{0}, and call these ‘clock-zero’ models, denoted by NV+1\mathbb{Z}_{N_{V}+1}.

Drawing on Equ (7), the generic coordinate-space Hamiltonian is

βH=D02[r{gL(T)S(r)2+ξ02|S(r)|2}+A12r,r,U(rr)S(r)S(r)],\begin{array}[]{rr}\beta H=\dfrac{D_{0}}{2}[\sum_{\vec{r}}\sum_{\ell}\{g_{L}(T){\vec{S}_{\ell}}(\vec{r})^{2}+\xi_{0}^{2}|\vec{\nabla}{\vec{S}}_{\ell}(\vec{r})|^{2}\}\\ +\dfrac{A_{1}}{2}\sum_{\vec{r},\vec{r}^{\prime}}\sum_{\ell,\ell^{\prime}}U_{\ell\ell^{\prime}}(\vec{r}-\vec{r}^{\prime}){\vec{S}}_{\ell}(\vec{r}){\vec{S}}_{\ell^{\prime}}(\vec{r}^{\prime})],\end{array} (13)

where the overall energy scale is D0(T)2ε¯2(T)E0/TD_{0}(T)\equiv 2{\bar{\varepsilon}^{2}}(T)E_{0}/{T}. Here ξ0\xi_{0} is the domain-wall thickness parameter, A1A_{1} is the elastic constant for the non-OP compressional strain R24 ; R25 ; R26 . The kernel UU_{\ell\ell^{\prime}} is an NOP×NOPN_{OP}\times N_{OP} matrix potential, that carries the spatial dimensionality d=3d=3, and depends on ratios of other non-OP elastic constants to A1A_{1}. Local meanfield treatmentsR22 yield even the complex strain textures of some real materials R13 ; R14 .

The generic k\vec{k} space Hamiltonian is obtained from S(r)=1NkS(k)eik.rS_{\ell}(\vec{r})=\frac{1}{\sqrt{N}}\sum_{\vec{k}}S_{\ell}(\vec{k})e^{i\vec{k}.\vec{r}}, and as S(r){\vec{S}}(\vec{r}) is real, S(k)=S(k){\vec{S}}({\vec{k}})^{*}={\vec{S}}(-{\vec{k}}). The Hamiltonian and energy-spectrum are

βH=D02k,ϵ(k,T)S(k)S(k);ϵ,(k,T)[{gL(T)+ξ02K2}δ,+A12U(k)].\begin{array}[]{rr}\displaystyle{\beta H=\frac{D_{0}}{2}\sum_{\vec{k}}\sum_{\ell,\ell^{\prime}}\epsilon_{\ell\ell^{\prime}}(\vec{k},T)S_{\ell}(\vec{k})S_{\ell^{\prime}}(\vec{k})^{*}};\\ \displaystyle{\epsilon_{\ell,\ell^{\prime}}(\vec{k},T)\equiv[\{g_{L}(T)+\xi_{0}^{2}{\vec{K}}^{2}\}\delta_{\ell,\ell^{\prime}}+\frac{A_{1}}{2}U_{\ell\ell^{\prime}}({\vec{k}})].}\end{array} (14)
Refer to caption
Figure 8: Angell-type plot as in glasses, for athermal martensites: The delay times t¯m(T){\bar{t}}_{m}(T) are replotted versus Td/TT_{d}/T, so that Arrhenius activated times would give a straight line. The x-axis data for the four transitions go from a value of unity on the left, to their respective Td/TT_{d}/T on the right. The obvious curvature shows that delays are not activated over energy barriers. They are attributed to entropy barriers.

,

The 3D transitions are given below in the sequence of NOP=1,2,2,3N_{OP}=1,2,2,3, plus NV=2,3,6,4N_{V}=2,3,6,4 cases respectively.

a) Tetragonal-Orthorhombic case (NOP=1,NV=2N_{OP}=1,N_{V}=2):
The scalar OP is the first deviatoric-strain OP e2=(exxeyy)/2e_{2}=(e_{xx}-e_{yy})/{\sqrt{2}}, with S\vec{S} having 2+12+1 values: at the origin, and pointing to the two endpoints of a unit-circle diameter. The Hamiltonian is like a 3D Spin-1 Blume Capel model R24 , but with anisotropic powerlaw interactions, and with the quadratic term fL(T)S2f_{L}(T)\vec{S}^{2} where fL(T)<0f_{L}(T)<0. The Hamiltonian is a clock-zero 2+1\mathbb{Z}_{2+1} model R21 .The scalar compatibility kernel U(k)U(\vec{k}) for the tetragonal-orthorhombic transition is given in Equ. (A26) of Ref 21.

With fL(T)ε¯2(T)gL(T)0f_{L}(T)\equiv{\bar{\varepsilon}}^{2}(T)g_{L}(T)\leq 0, the Tetragonal-orthorhombic (and also 2D square-rectangle) case has the squared-mean OP and gL(T)g_{L}(T) factor as R21

ε¯2(T)=(2/3)[1+(13τ/4)];gL(T)=(τ1)+(ε¯21)2.\begin{array}[]{rr}\displaystyle{{\bar{\varepsilon}}^{2}(T)=(2/3)[1+\sqrt{(}1-3\tau/4)]};\\ \displaystyle{g_{L}(T)\equiv=(\tau-1)+({\bar{\varepsilon}}^{2}-1)^{2}}.\end{array} (15)

b) Cubic-tetragonal case (NOP=2,NV=3N_{OP}=2,N_{V}=3):
This 3D transition has been considered earlierR23 ; R31 . The OP strains are the two deviatoric strains (e3,e2)=({2ezzexxeyy}/6,{exxeyy}/2)(e_{3},e_{2})=(\{2e_{zz}-e_{xx}-e_{yy}\}/{\sqrt{6}},\{e_{xx}-e_{yy}\}/{\sqrt{2}}). The spin values S=(S3,S2)\vec{S}=(S_{3},S_{2}) vectors are in a plane in OP space, with S\vec{S} having 3+13+1 values: at the origin and pointing to the three corners of a triangle inscribed in a unit circle. The Hamiltonian is a clock-zero 3+1\mathbb{Z}_{3+1} model R21 .The compatibility kernel is a 2×22\times 2 matrix, U(k)U_{\ell\ell^{\prime}}({\vec{k}}), with ,=2,3\ell,\ell^{\prime}=2,3, as in Equ (A23) of Ref 21.

The mean OP and gL(T)g_{L}(T) of the cubic-tetragonal transition are

ε¯(T)=(3/4)[1+(18τ/9)];gL(T)=(τ1)+(ε¯1)2.\begin{array}[]{rr}\displaystyle{{\bar{\varepsilon}}(T)=(3/4)[1+\sqrt{(}1-8\tau/9)]};\\ \displaystyle{g_{L}(T)=(\tau-1)+({\bar{\varepsilon}}-1)^{2}}.\end{array} (16)

c) Cubic-orthorhombic case (NOP=2,NV=6N_{OP}=2,N_{V}=6):
The OP strains are again the two deviatoric strains (e3,e2)(e_{3},e_{2}) as above. The nonzero S=(S3,S2)\vec{S}=(S_{3},S_{2}) spin vectors are in a plane in OP space, with S\vec{S} having 6+16+1 values: at the origin and pointing to the six corners of a hexagon inscribed in a unit circle. The Hamiltonian is a clock-zero 6+1\mathbb{Z}_{6+1} model R21 . The Compatibility kernel is a 2×22\times 2 matrix U,(k){U_{\ell,\ell^{\prime}}}(\vec{k}), again with ,=2,3\ell,\ell^{\prime}=2,3 and is the same as the cubic-tetragonal case, given in Equ (A23) of Ref 21.

The squared-mean OP and gL(T)g_{L}(T) for the Cubic-orthorhombic case, are the same as the tetragonal-orthorhombic in Equ (15).

d) Cubic-trigonal case (NOP=3,NV=4N_{OP}=3,N_{V}=4):
The three OP for the cubic-trigonal transition are the three shears e4,e5,e6=exy,eyz,ezxe_{4},e_{5},e_{6}=e_{xy},e_{yz},e_{zx}, and the variant vector has three vector components, with S\vec{S} having 4+14+1 values: at the origin and pointing to the four corners of a tetrahedron inscribed in a unit sphere. The Compatibility kernel is now a 3×33\times 3 matrix U,(k)U_{\ell,\ell^{\prime}}(\vec{k}), with ,=4,5,6\ell,\ell^{\prime}=4,5,6, or six components U44,U55,U66,U45,U54,U64U_{44},U_{55},U_{66},U_{45},U_{54},U_{64} as in Equ. (A20) of Ref 21.

The mean OP and gL(T)g_{L}(T) for the cubic-trigonal case are the same as the cubic-tetragonal case in Equ (16).

IV Monte Carlo Simulations:

Simulations were done on models for four transitions in 3D. The initial state t=0t=0 is 2%2\% randomly and dilutely seeded martensite cells, in an austenite sea of S=0\vec{S}=0. Evolutions proceed at quench temperatures T<T0T<T_{0}. Typical parameters are T0=1T_{0}=1; ξ02=1\xi_{0}^{2}=1; Tc=0.81T_{c}=0.81 to 0.970.97; A1=1A_{1}=1 to 8585; E0=3,4,5,6E_{0}=3,4,5,6; N=L3=163N=L^{3}=16^{3}; Nruns=100N_{runs}=100; and holding times th=104t_{h}=10^{4} MC sweeps, each over NN sites.

The Compatibility kernels arise from the non-OP harmonic terms, with (6NOP)(6-N_{OP}) elastic constants. For all transitions, we specify the fixed ratio of other non-OP elastic constants, to A1A_{1}. For the tetragonal-orthorhombic transition, with NOP=1N_{OP}=1 and S2S_{2} as the OP spin, the non-OP elastic constants are the other deviatoric constant A3A_{3}, and the three shear constants A4,A5,A6A_{4},A_{5},A_{6}, set to be A3=A4=A5=A6=A1/2A_{3}=A_{4}=A_{5}=A_{6}=A_{1}/2. Similarly, for the cubic-tetragonal and cubic-orthorhombic cases with NOP=2N_{OP}=2 and (S3,S2)(S_{3},S_{2}) as the OP spins, the non-OP constants are set to be A4=A5=A6=A1/2A_{4}=A_{5}=A_{6}=A_{1}/2. Finally, for the cubic-trigonal case with NOP=3N_{OP}=3 and the shears (S4,S5,S6)(S_{4},S_{5},S_{6}) as the OP, the constants are set as A2=A3=A1/2A_{2}=A_{3}=A_{1}/2.

The standard MC procedure R32 is followed, with an extra data retention R1 ; R2 ; R3 ; R4 of energy changes.
0. Take NN lattice sites, each with a vector spin of NOPN_{OP} components, in one of NV+1N_{V}+1 possible values (including zero) at MC time tt. Each {S(r)}\{{\vec{S}}(\vec{r})\} set is a ‘configuration’. With nm=0n_{m}=0 or 11 for uniform austenite or martensite, the average martensite fraction is nm(t)1n_{m}(t)\leq 1. The conversion time tmt_{m} is defined as when R24 nm(tm)=1/2n_{m}(t_{m})=1/2.
1. Randomly pick one of NN sites, and randomly flip the spin on it to a new direction/value, and find the (positive or negative) energy change δE\delta E.
2. If δE0\delta E\leq 0, then accept the flip. If δE>0\delta E>0, then accept flip with probability eδE/Te^{-\delta E/T}. Record this spin-flip δE\delta E, that is usually not retained after use.
3. Repeat steps 1 and 2. Stop after NN such spin-flips. This is the t+1t+1 configuration with nm(t+1)n_{m}(t+1).
4. We collect all recorded {δE}\{\delta E\} over each MC sweep of every run while tracking nm(t)n_{m}(t). The collection is only up to a waiting time equal to the martensite conversion time. t=twtm(T)th.t=t_{w}\leq t_{m}(T)\leq t_{h}. We do six quenches, from T=T1T=T_{1} upwards to TdT_{d}.

A single-variant athermal martensite droplet or ‘embryo’ R11 can form anywhere, and after a local conversion at a waiting time tw=tmt_{w}=t_{m}, can propagate rapidly to the rest of the system R11 ; R19 . Hence it is the mean rates r¯m{\bar{r}}_{m} (or inverse times), that are averaged over NrunN_{run} runs, analogous to total resistors in parallel determined by the smallest resistance. The mean times t¯m{\bar{t}}_{m} are defined as the inverse mean ratesR24 .

r¯m(T)=1Nrunn=1Nrun1tm(n);t¯m(T)1r¯m(T).{\bar{r}}_{m}(T)=\frac{1}{N_{run}}{\sum_{n=1}}^{N_{run}}\frac{1}{t_{m}(n)};~{}~{}{\bar{t}}_{m}(T)\equiv\frac{1}{{\bar{r}}_{m}(T)}. (17)

For an un-successful nn-th run that does not convert in a holding time tht_{h}, the rate rm(n)r_{m}(n) could be assigned a value of either 1/th1/t_{h} (conversion right after cutoff) or 0 (conversion never occurs). We choose the 1/th1/t_{h} cutoff, that shows up as a flattening of the mean rate near TdT_{d}. An extrapolation of the linear part of rm(T)r_{m}(T) to the temperature axis yields a valueR24 for TdT_{d}.

Refer to caption
Figure 9: Bottlenecks in phase space for different transitions: Four-panel plot shows energy contours on 2D slices of the 3D bottleneck, with δ0(T)=0.1,0,+0.1,+0.2\delta_{0}(T)=-0.1,0,+0.1,+0.2. The sizes decrease on warming, and the bottleneck inner radius is seen to pinch off, at some Td{T_{d}}^{\prime}. The contours are a) Tetragonal-orthorhombic, Td=0.69{T_{d}}^{\prime}=0.69 b) Cubic-tetragonal, Td=0.60{T_{d}}^{\prime}=0.60; c) Cubic-orthorhombic Td=0.60{T_{d}}^{\prime}=0.60; d) Cubic-trigonal Td=0.70{T_{d}}^{\prime}=0.70. The corresponding delay-divergence temperatures Td=0.75,0.59,0.69,0.75T_{d}=0.75,0.59,0.69,0.75 are close in value, and taken as the same, for simplicity of discussion.
Refer to caption
Figure 10: Bottleneck inner and outer radius: Four-panel plot showing kouter2(T)k_{outer}^{2}(T) (solid), kinner2(T)k_{inner}^{2}(T) (dashed) lines versus temperature TT, for transitions in the order a) to d) as in Fig 9. The inner radius vanishes close to the delay-divergence TdT_{d} (downward arrows). The outer radius vanishes at the thermodynamic transition temperature T0=1T_{0}=1. It intersects the horizontal light dashed line denoting a Brillouin Zone scale π2\pi^{2}, at temperatures close to the T1=0.51,0.21,0.4,0.31T_{1}=0.51,0.21,0.4,0.31 for explosive conversions (downward arrows)

V Delays and bottlenecks:

For the four transitions, we consider i) Delays from sluggish Domain Walls; ii) Bottlenecks in Fourier space.

V.1 Delays from sluggish Domain Walls

Figure 2 shows the twinned microstructures in all four transitions, colour coded through the variant-label VV, where V=0V=0 is always austenite. For the single-OP tetragonal-orthorhombic transition, V=±1V=\pm 1 has two variant colours. For the two-component OP, the cubic-tetragonal and cubic-orthorhombic transitions have respectively, V=1,2,3V=1,2,3 and V=1,2,6V=1,2,...6 variant colours. For the three-component OP, the cubic trigonal has V=1,2,3,4V=1,2,3,4 four variant colours. Fig 2 shows that all allowed degenerate NVN_{V} variants are present, for all four transitions.

The tetragonal-orthorhombic, and cubic-tetragonal twins can have Domain Walls decorated with austenite, as also found in the 2D case R25 . Such observed austenite retentionsR11 can be understood: they are energetically favoured, when the lower Ginzburg costs of austenite-martensite walls compensate for the absence of the negative condensation energy fL(T)<0f_{L}(T)<0 of martensite unit cells. As TT is lowered, the energy accounting is reversed, and the austenite inclusions are expelled, replaced by martensite, so DW are only between martensite variants R25 .

We define a fractional deviation from a characteristic temperature TdT_{d}, as

δ0(T)(TTd)/Td0.\delta_{0}(T)\equiv(T-T_{d})/T_{d}\leq 0. (18)

Figure 3 shows the martensite conversion-fraction nm(t)n_{m}(t) versus MC time tt in a single run, for different δ0(T)\delta_{0}(T). For quenches to below T=T1T=T_{1}, there is an immediate avalanche conversion in a single t=1t=1 sweep, characteristic of athermal martensite. For temperatures T>T1T>T_{1} there is a strange ‘incubation’ behaviour, or a postponement of these avalanches. The fraction nm(t)n_{m}(t) remains virtually unchanged, up till t=tmt=t_{m} when nm(t)n_{m}(t) rises sharply through 1/21/2, to unity. The cubic-trigonal transition has NOP=3N_{OP}=3 order parameter components, NV=4N_{V}=4 variants, and can show unusual behaviour. Here, there is an initial jump to nm=1/2n_{m}=1/2 followed by incubation, and then a jump to unity.

Fig 4 shows that for T<T1T<T_{1} there is an immediate spike in the MC acceptance fraction Aacc(t)A_{acc}(t) at t=1t=1, and drop in energy E(t)E(t) to negative values. For T>T1T>T_{1}, during incubations they both remain zero, up to t=tm(T)t=t_{m}(T), when the acceptance spikes and the energy drops. Again, the cubic-trigonal case is unusual.

What goes on microscopically, during incubation ? In 2D, Video R27 A shows random initial seeds of both variants (red,blue) can quickly form an almost zero energy single-variant martensitic droplet or embryo (red) in an austenite background (green), in the DW Vapour state. The small droplet extends and retracts amoeba-like arms, searching for energy-lowering pathways. After a long conversion delay tmt_{m} of hundreds of time steps, when nm0n_{m}\simeq 0, the single-variant droplet (red) suddenly expands rapidly and generates the opposite variant (blue). This is the wandering-wall or DW Liquid state. After a shorter orientation delay, the walls of the DW Liquid orient to a DW crystal.

Figure 5 shows for all four transitions, the mean fraction of successful conversions Φm\Phi_{m} during a holding time t=tht=t_{h} over 100 runs, versus the temperature deviation δ0(T)\delta_{0}(T). For temperatures δ00.1\delta_{0}\leq-0.1, every run converts, and Φm=1\Phi_{m}=1. However, for δ0>0.1\delta_{0}>-0.1, Φm(T)\Phi_{m}(T) falls through 1/2 at δ0(T)0.05\delta_{0}(T)\sim-0.05, and then to zero. The success fraction is not exponentially sensitive to overall energy scales E0=3,4,5,6E_{0}=3,4,5,6, so the probability of conversion is not activated over an energy barrier.

Just above TdT_{d} there are unsuccessful runs (not shown), when the martensite seeds can dissolve back into austenite. The seeds will not be regenerated, even if the holding time tht_{h} is increased, or if the temperature is loweredR20 .

Figure 6 shows a linear-linear plot of the mean conversion times t¯m{\bar{t}}_{m} versus δ0(T)\delta_{0}(T) for various E0E_{0}. The absence of exponential sensitivity to E0E_{0} implies the delays are not activated over energy barriers, but are due to entropy barriers. For T<T1T<T_{1} fluctuations are small, while for T>T1T>T_{1} standard-deviation error bars ±σ\pm\sigma over the Nrun=100N_{run}=100 runs, are larger, on approaching TdT_{d}.

If the probability of entropy-barrier crossings coming from a product of sequential random steps, a logarithm of rates would be an additive random variable, suggesting a log-normal distribution of rates R25 P(rm)P(r_{m}). Fig 7 shows optimized-bin histograms R37 of rmr_{m} data, with (asymmetric) log-normal lines as guides to the eye. Although data are too sparse to decide distributions, clearly fast conversions are narrow, and slow conversions are broad, similar to protein folding R29 ; R30 .

Fig 8 shows an Angell-type plot R8 of log delay time versus Td/T>1T_{d}/T>1. Arrhenius-type activations over energy barriers would be linear. The delays have curvatures, and so must be from entropy barriers.The solid curve is VFT behaviour of Equ (29) below, with B0=0.25B_{0}=0.25.

V.2 Bottlenecks in Fourier-space:

We draw on concepts of protein folding R28 ; R29 ; R30 , to understand the entropy barrier delays.

A purely random search of protein configurations could take astronomical times (Leventhal paradox). Rapid protein folding is attributed to a configuration-space Golf Hole (GH) opening into a Funnel of negative-energy configurations, leading rapidly to the folded protein state R28 ; R29 . Bicout and Szabo R30 consider a random walk of a Brownian particle in a space of eigen-labels of protein folding modes (that could be analogous to propagative martensitic twinning modesR38 ). The Brownian particle has to locate and enter spherical zero-energy GH contour of marginal modes. Unusual delays can occur, at the GH edge.

Refer to caption
Figure 11: Fluctuation ratios R0R_{0} of forward/ backward energy change probabilities in log-linear plot: Four-panel plot for all transitions, of the ratio R0(δE,T)P0(δE,T)/P0(δE,T)R_{0}(\delta E,T)\equiv P_{0}(\delta E,T)/P_{0}(-\delta E,T) versus MC energy change δE\delta E, for six TT.
Refer to caption
Figure 12: Even-symmetry prefactor P0(+)P^{(+)}_{0} in linear-linear plot: Four-panel plot for all transitions, checking that the log-linear prefactor P0(+)(δE,T)P^{(+)}_{0}(\delta E,T) versus energy change δE\delta E has no linear contribution near the origin.
Refer to caption
Figure 13: Variance of the even-symmetry prefactor : Four-panel linear-linear plot of the variance σ2(T)\sigma^{2}(T), of the prefactor P0(+)(δE,T)P_{0}^{(+)}(\delta E,T), versus Teff(T)/M(T)T_{eff}(T)/M(T) for the four transitions. The energy scale is chosen as the (positive) mean energy change M(T)<δE>M(T)\equiv<\delta E> over the entire PES distribution.

In our case, the bottleneck is fixed by the energy spectrum from Equ (14) in 3D Fourier space (taken as diagonal in \ell, for discussion):

ϵ(k,T)=ξ02K(k)2|gL(τ)|+(A1/2)U(k^).\epsilon_{\ell\ell}(\vec{k},T)=\xi_{0}^{2}{{\vec{K}}(\vec{k})}^{2}-|g_{L}(\tau)|+(A_{1}/2)U_{\ell\ell}(\hat{k}).~{}~{} (19)

Energy spectra set to a constant CC or ϵ(k,T)=C\epsilon_{\ell\ell}(\vec{k},T)=C, define contours in k\vec{k}-space. The Ginzburg term at long wavelengths k2\sim\vec{k}^{2}, forms a k\vec{k}-space spherical bowl in 3D, with zero-energy minimum at the origin. The Compatibility term U(k^)U_{\ell\ell}(\hat{k}) angularly modulates its 2D surface to produce an anisotropic zero-energy contour R24 .

The phase-space boundary ϵ(k,T)=0\epsilon_{\ell\ell}(\vec{k},T)=0 separates an outside k\vec{k} region of positive (austenite) energies, from a k\vec{k}-region inside, of (martensitic) negative energies. Video B shows R27 a 2D circular droplet Fourier profile in (kx,ky)(k_{x},k_{y}) as it distorts, to enter the phase space bottleneck.

We consider spectra with ϵ22(k,T)\epsilon_{22}(\vec{k},T) for the first three transitions, and ϵ66(k,T)\epsilon_{66}(\vec{k},T) for the cubic-trigonal case. Consistent with the twin orientations in Fig 1, the plane intersecting the 3D bottleneck to yield a 2D cross-section is taken as [k^x,k^y,k^z]=[1,1,1][{\hat{k}}_{x},{\hat{k}}_{y},{\hat{k}}_{z}]=[1,1,1]. The plane through the Brillouin Zone origin is kx+ky+kz=0k_{x}+k_{y}+k_{z}=0, and Fig 9 shows for all four transitions, the TT-dependent contours of constant ϵ(kx,ky,kz=kxky,T)\epsilon_{\ell\ell}(k_{x},k_{y},k_{z}=-k_{x}-k_{y},T) versus (kx,ky)k_{x},k_{y}) for temperature range δ0(T)=0.1\delta_{0}(T)=-0.1 to +0.2+0.2.As mentioned, the cubic-tetragonal and cubic-orthorhombic have the same kernel but different Landau factor gL(T)g_{L}(T), so one would expect the second and third panels to show the same overall shapes, but slightly different energy contours for a given TT: this is indeed the case.

The bottleneck sizes are large at low TT and small at high TT. The contours are angularly modulated between a smaller inner-radius wave-vector kinner(T)k_{inner}(T) and larger outer-radius wave-vector kouter(T)k_{outer}(T). From the spectrum Equ (19)

kouter2(T)=ξ02[|gL(T)|(A1/2)U(min)];kinner2(T)=ξ02[|gL(T)|(A1/2)U(max)].\begin{array}[]{rr}\displaystyle{k_{outer}^{2}(T)={\xi_{0}}^{-2}[|g_{L}(T)|-(A_{1}/2)U_{\ell\ell}(min)]};\\ \displaystyle{k_{inner}^{2}(T)={\xi_{0}}^{-2}[|g_{L}(T)|-(A_{1}/2)U_{\ell\ell}(max)].}\end{array} (20)

For U(min)=0U_{\ell\ell}(min)=0, the outer square-radius vanishes at the Landau temperature, kouter2(T0)=|gL(T0)|=0k_{outer}^{2}(T_{0})=|g_{L}(T_{0})|=0. Close to transition,

kouter2(T)b(T0)(TT0)k_{outer}^{2}(T)\simeq b(T_{0})(T-T_{0}) (21)

where the Taylor expansion coefficient b(T)dgL(T)/dT<0b(T)\equiv-dg_{L}(T)/dT<0.

With a positive U,(max)>0U_{\ell,\ell}(max)>0 there is a temperature Td<T0T_{d}<T_{0} where the inner radius can pinch off to zero, kinner2(Td)=|gL(Td)|(A1/2)U,(max)=0k_{inner}^{2}(T_{d})=|g_{L}(T_{d})|-(A_{1}/2)U_{\ell,\ell}(max)=0, while the outer radius is still nonzero. Near TdT_{d},

kinner2(T)=|gL(T)||gL(Td)|b(Td)(TTd].\begin{array}[]{rr}\displaystyle{k_{inner}^{2}(T)=|g_{L}(T)|-|g_{L}(T_{d})|}\\ \displaystyle{\simeq b(T_{d})~{}(T-T_{d}]}.\\ \end{array} (22)

Figure 10 shows the inner and outer squared-radii, both almost linear, and vanishing respectively at TdT_{d} and T0T_{0}.

The conversion-delay divergence comes from a pinch-off of the inner radius kinner(T)k_{inner}(T) of the bottleneck. The topology of a 2D slice of the 3D negative energy states, goes from an open butterfly to a segmented four-petalled flower R25 . It is impossible for the broad Fourier profile of a small droplet to distort at zero total energy, into four separated petal-like segments. The lower-energy states for T>TdT>T_{d} are thus available, but not accessible. The intershell configurational pathway closes; the success-fraction vanishes; and the entropy barrier diverges.

VI PES signatures in all four transitions

We now exhibit PES signatures in the four athermal martensite transitions. Entropy barriers are insensitive to energy scales, so we consider only E0=3E_{0}=3.

Refer to caption
Figure 14: Normalized probabilities P0P_{0} of energy-changes in linear-linear plot: Four-panel Figure for all transitions, showing the probability P0(δE,T)P_{0}(\delta E,T) versus energy change δE\delta E for the six quench temperatures TT in the legend.The probabilities are consistent with the predicted PES signature of shifted Gaussians peaked near a mean energy changes M(T)>0M(T)>0, with exponential heat-loss tails for δE<0\delta E<0.
Refer to caption
Figure 15: Normalized probability of energy-changes P0P_{0} in log-linear plot : Four-panel Figure for all transitions, showing a log-linear version of Fig 14 on a zoomed in scale of P0(δE,T)P_{0}(\delta E,T) versus energy change δE\delta E, at the same six temperatures TT.The linear behaviour is a PES signature, with slopes determining the inverse effective temperatures, βeff/21/2Teff\beta_{eff}/2\equiv 1/2T_{eff}, that flatten near T=T1T=T_{1}.

As noted the MC procedures of Section IV retain the set of single spin-flip energy changes {δE}\{\delta E\} from all N spin-flips, in each of NrunN_{run} runs, up to t MC times ttm(T)t\leq t_{m}(T). The histograms can be dense since the data set size can be large: N×tm×NrunN\times{t}_{m}\times N_{run} has up to 163×104×10016^{3}\times 10^{4}\times 100 data points.

An ageing-state fluctuation relation is postulated R4 . The probability P0(δE,T)P_{0}(\delta E,T) to hit configurations EE^{\prime} from EE, is proportional to the target size, or the number of accessible states: P0(δE,T)Ω(E)P_{0}(\delta E,T)\sim\Omega(E^{\prime}), with S(E)=lnΩ(E)S(E^{\prime})=\ln\Omega(E^{\prime}), where E=E+δE<EE^{\prime}=E+\delta E<E. The reverse path has P0(δE,T)Ω(E)P_{0}(-\delta E,T)\sim\Omega(E). The ratio of forward and backward probabilities R0(δE)R_{0}(\delta E) is related to the entropy change and entropy barrier ΔS(δE)S(E)S(E)SB<0\Delta S(\delta E)\equiv S(E^{\prime})-S(E)\equiv-S_{B}<0. Thus

R0P0(δE,T)P0(δE,T)=Ω(E)Ω(E)=eΔS(δE).R_{0}\equiv\frac{P_{0}(\delta E,T)}{P_{0}(-\delta E,T)}=\frac{\Omega(E^{\prime})}{\Omega(E)}=e^{\Delta S(\delta E)}. (23)

Fig 11 shows four-panel log-linear plots of the fluctuation ratio R0(δE,T)R_{0}(\delta E,T). Since R0(δE)R0(δE)1R_{0}(\delta E)R_{0}(-\delta E)\equiv 1, the entropy change is odd, ΔS(δE)+ΔS(δE)=0\Delta S(\delta E)+\Delta S(-\delta E)=0, and a solution is

P0(δE,T)=P0(+)(δE,T)e12ΔS(δE),P_{0}(\delta E,T)={P_{0}}^{(+)}(\delta E,T)~{}e^{\frac{1}{2}\Delta S(\delta E)}, (24)

where the (even) prefactor is the geometric mean, P0(+)(δE,T)=P0(δE,T)P0(δE,T){P_{0}}^{(+)}(\delta E,T)=\sqrt{P_{0}(\delta E,T)P_{0}(-\delta E,T)}. For small energy changes, S(E+δE)S(E)βeffδES(E+\delta E)-S(E)\simeq\beta_{eff}\delta E, and hence P0(δE,T)P0(+)(0,T)e12βeff(T)δEP_{0}(\delta E,T)\simeq{P_{0}}^{(+)}(0,T)~{}e^{\frac{1}{2}\beta_{eff}(T)\delta E}.

Fig 12 is just a check that the prefactor P0(+)(δE,T)P^{(+)}_{0}(\delta E,T) versus δE\delta E has no linear contribution near the origin, that might modify the exponential tail. For temperatures near T1T_{1} it is a single-peak gaussian, while near TdT_{d} it can go bimodal.

Fig 13 shows that the variance σ2\sigma^{2} of the weight P0(+)(δE,T){P_{0}}^{(+)}(\delta E,T) versus a scaled Teff(T)T_{eff}(T) is linear and nonsingular, for all four transitions.

Fig 14 shows four-panel linear-linear plots of (normalized) P0(δE,T)P_{0}(\delta E,T) versus δE\delta E for four transitions, each at one of six temperatures in the Legend. The peak is at positive energy as in the oscillator case R2 , and moves left as TT decreases towards T1T_{1}. The exponential tails near the origin are barely visible.

Fig 15 shows the same four plots but now in log-linear form, and zoomed in. The curves all show the PES signature of linearity around the origin δE=0\delta E=0. The cubic tetragonal panel has been shown earlier R31 . As TT is lowered to T1T_{1}, the slopes βeff(T)/2\beta_{eff}(T)/2 all flatten.

Refer to caption
Figure 16: Effective temperature (and its inverse) versus quench temperature: Four-panel Figure for all transitions, showing effective search temperature on the left vertical axis versus TT. For all transitions, the TeffT_{eff} vanishes linearly TdT\sim T_{d}-T at a search-freezing temperature TdT_{d}. The inverse βeff(T)\beta_{eff}(T) on the right vertical axis vanishes linearly TT1\sim T-T_{1} at a search explosion temperature T1T_{1}.
Refer to caption
Figure 17: Four panel plot of scaled probability of energy change Π0\Pi_{0} versus z=βeffδE/2z=\beta_{eff}\delta E/2. The four transitions in panels a),b),c),d) have respective slope mean values and standard deviations of 1.000±0.045;1.025±0.036;1.009±0.08;0.850±0.0851.000\pm 0.045;~{}1.025\pm 0.036;~{}1.009\pm 0.08;~{}0.850\pm 0.085.

Fig 16 shows a central result, namely the search temperature Teff(T)T_{eff}(T) and its inverse, βeff(T)\beta_{eff}(T) versus TT. The left-axis search temperature Teff(T)T_{eff}(T) intersects the temperature axis at an extrapolated Teff(Td)=0T_{eff}(T_{d})=0, defining a quench temperature TdT_{d}. The vanishing appears to be linear, Teff(T)TdTT_{eff}(T)\sim T_{d}-T.

The mean conversion rate involves an integral over the heat releases of the distribution R39 . The mean time is then a singular exponential t¯mt0eM/4Tefft0eB0Td/(TdT){\bar{t}}_{m}\simeq t_{0}e^{M/4T_{eff}}\simeq t_{0}e^{B_{0}T_{d}/(T_{d}-T)}. The Vogel Fulcher-Tammann form R5 ; R7 ; R8 thus emerges naturally from a search temperature freezing inducing a rapid arrest of PES cooling, and an entropy-barrier divergence.

Similarly, the inverse effective temperature βeff(T)\beta_{eff}(T) on the right-axis of Fig 16 seems to go to zero linearly (TT1)\sim(T-T_{1}) at a search explosion T1T_{1} where entropy barriers vanish.

Once again, the cubic-trigonal last panel is unusual, with TeffT_{eff} showing a smaller slope near TdT_{d}. If the linear slope actually vanishes as Teff(T)(TTd)2T_{eff}(T)\sim(T-T_{d})^{2} then that would yield ‘super-VFT’ behaviour R5 , tme1/(TTd)2t_{m}\sim e^{1/(T-T_{d})^{2}}.

Fig 17 shows the scaled ratio of occurrence probability to its value at the origin, Π0P0(δE,T)/P0(0,T)\Pi_{0}\equiv P_{0}(\delta E,T)/P_{0}(0,T) versus zβeffδE/2δS/2z\equiv\beta_{eff}\delta E/2\simeq\delta S/2. The dashed white lines have slopes close to the predicted universal slope of unity, as given in the Figure caption.

The normalized probability PMCP_{MC} of a Monte Carlo spin-flip is the product of the occurrence probability P0P_{0} and an MC acceptance factor with step functions,

PMC(δE,T)=P0(δE,T)NMC(T)[θ(δE)+eδE/Tθ(δE)],P_{MC}(\delta E,T)=\frac{P_{0}(\delta E,T)}{N_{MC}(T)}[\theta(-\delta E)+e^{-\delta E/T}\theta(\delta E)], (25)

with NMC(T)N_{MC}(T) a normalization constant. The ratio of the MC probability and its value at the origin defines ΠMC(δE,T)[PMC(δE,T)/PMC(0,T)]\Pi_{MC}(\delta E,T)\equiv[P_{MC}(\delta E,T)/P_{MC}(0,T)]. With zβeff(T)δE/2z\equiv\beta_{eff}(T)\delta E/2,

ΠMC[ezθ(δE)+ez[(2Teff/T)1]θ(δE)]/NMC(T).\Pi_{MC}\simeq[e^{z}\theta(-\delta E)+e^{-z[(2T_{eff}/T)-1]}\theta(\delta E)]/N_{MC}(T). (26)

Fig 18 shows a log-linear plot of ΠMC\Pi_{MC} along the positive axis z=βeffδE/2>0z=\beta_{eff}\delta E/2>0. The closeness of data to theoretical lines with slope [12Teff/T)]<0[1-2T_{eff}/T)]<0 is further evidence for PES.

Refer to caption
Figure 18: Four panel plot of ΠMC\Pi_{MC} versus z=βeffδE/2>0z=\beta_{eff}\delta E/2>0. The light theoretical line of slope [12Teff/T)][1-2T_{eff}/T)] has a reasonable match to data.

In conclusion all four transitions show PES signatures, lending support to the Partial Equilibration Scenario.

VII PES delays in simulations and experiment

We show that delay data both in simulations and in experiment, are consistent with a picture of diverging entropy barriers from linearly vanishing PES effective temperatures.

VII.1 VFT delays in 3D simulations

Refer to caption
Figure 19: Vogel-Fulcher-like behaviour in simulations: Four-panel plot of scaled data in simulations of log-linear scaled t¯m/t0{\bar{t}}_{m}/t_{0} versus scaled B0/|δ0(T)|B_{0}/|\delta_{0}(T)|, for the four transitions a),b),c), d), with each panel showing E0=3,4,5,6E_{0}=3,4,5,6. Data clustering for small |δ0(T)||\delta_{0}(T)|, on the dashed line over three orders of magnitude is evidence for Vogel-Fulcher behaviour. For lower temperatures, there is a peel-off towards the x-axis near T=T1T=T_{1} (downward arrow).

Vogel-Fulcher-Tamman temperature dependences can be written near TdT_{d} as

t¯m(T)=t0eB0Td/|TTd|=t0eB0/|δ0(T)|{\bar{t}}_{m}(T)=t_{0}e^{B_{0}T_{d}/|T-T_{d}|}=t_{0}e^{B_{0}/|\delta_{0}(T)|} (27)

where t0,B0Tdt_{0},B_{0}T_{d} are the time and energy scales, for DW shifts of a lattice spacing.

The logarithms of VFT times can be written in two useful forms, to extract constants B0,t0B_{0},t_{0} from simulations and experiments. Thus

1lnt¯m(T)=(|δ0(T)|/B0)[1+(logt0)(|δ0(T)|/B0)]\frac{1}{\ln{{\bar{t}}_{m}(T)}}=\frac{(|\delta_{0}(T)|/B_{0})}{[1+(\log{t_{0}})(|\delta_{0}(T)|/B_{0})]} (28)

and

lnt¯m(T)=logt0+[B0/|δ0(T0)|].\ln{{\bar{t}}_{m}(T)}=\log t_{0}+[B_{0}/|\delta_{0}(T_{0})|]. (29)

For simulations, B0B_{0} and t0t_{0} can be extracted from data using Equ (28) and Equ (29). Fig 19 shows for all four transitions, the data in a scaled form of

ln(t¯m/t0)=B0/|δ0(T)|.\ln({\bar{t}}_{m}/t_{0})=B_{0}/|\delta_{0}(T)|. (30)

There is data clustering around the Vogel-Fulcher straight line showing universality over 3 orders of magnitude near TdT_{d}. There is also a peel-off toward shorter times, near T1T_{1} (downward arrow).

VII.2 VFT delays in martensitic alloys

Delayed athermal martensitic transformations in metallic alloys have been tracked by conversion diagnostics suited to the scale of the waiting timesR16 ; R17 ; R18 such as electrical resistivity drops; or surface optical or X-ray reflectivity. In pioneering experiments, Kakeshita et al R17 used resistivity drops to detect the austenite to martensite delayed conversions for alloys FexNi1xFe_{x}Ni_{1-x}. The alloying percentage 100x100~{}x is 29.9,31.6,32.1%29.9,31.6,32.1\%, with start temperatures of Ms=239,177,148M_{s}=239,177,148 K.The delays discovered were of macroscopically long times. Other work such as the Klemradt groupR16 ; R18 on NiAlNiAl alloy delays, also rose rapidly: for temperature increments above the MsM_{s} values of 0.10.1 K, 0.60.6 K and 0.7K0.7K, the delay times went from R18 several seconds, to 10410^{4} seconds, to forever.

The data analysis of simulations is used again for experiment, as now described in more detail. To extract divergence temperatures TdT_{d} from simulation or experimental data, we plot 1/ln(t)1/\ln(t) versus TT, and extrapolateR24 straight line segments to the x-axis (not shown). For FeNi dataR17 this yields Td247,187,158T_{d}\simeq 247,187,158 K, well above MsM_{s}, with large fractional delay windows |δ0(Ms)|=|TdMs|/Td=0.03,0.05,0.06|\delta_{0}(M_{s})|=|T_{d}-M_{s}|/T_{d}=0.03,0.05,0.06. Similarly extrapolation of data for the NiAl alloyR18 with Ms=282.2M_{s}=282.2K yields Td=283KT_{d}=283K but with a smaller window |δ0(Ms)|3×103|\delta_{0}(M_{s})|\simeq 3\times 10^{-3}.

Another group considered NiTi alloys R20 , and argued that if the largest delay is at T=T0T=T_{0}, then for a long enough annealing time, conversions should be seen at any TT in a wide window Ms<T<T0M_{s}<T<T_{0}. However no conversion was detected, for holding at T=275.9T=275.9 above Ms=274.3KM_{s}=274.3K, for th=21t_{h}=21 days. The absence of conversion was attributed to a sparseness of (atomic) catalyst fields in facilitation-type delay models R20 . In our picture this absence could also be due to TT being outside the narrower conversion window Ms<T<Td<T0M_{s}<T<T_{d}<T_{0},

Fig 20 shows measurement data of conversion times tt, in seconds, versus temperature TT in degrees Kelvin. The left column shows a linear-linear plot like Equ (28) of 1/lnt1/\ln{t} versus |δ0(T)||\delta_{0}(T)| to extract slope 1/B01/B_{0} from Kakeshita data R17 for three alloys of FeNi (top panel); and from Klemradt dataR18 for a NiAl alloy (bottom panel). The right column shows a linear-linear plot Equ (29) of lnt\ln{t} versus 1/|δ0(T)1/|\delta_{0}(T), using lines of the extracted slope B0B_{0}, to determine the intercept lnt0\ln t_{0} for FeNi (top panel) and for NiAl (bottom panel). Downward arrow marks T1=T_{1}= for NiAl data. The ‘fragility’ R8 parameter B0Td=1.23KB_{0}T_{d}=1.23K, and a basic time scale for DW hops is t0=1t_{0}=1 second.

Refer to caption
Figure 20: Vogel-Fulcher-like behaviour in experiment: Left column shows data from both groups R16 ; R17 ; R18 , in a 1/ln(t)1/\ ln(t) versus |δ0(T)||\delta_{0}(T)| plot. The slope 1/B01/B_{0} is extracted from a fit to y=(1/B0)xy=(1/B_{0})x. Right column again shows results of both groups, in a log-linear plot of lnt¯m\ln{\bar{t}}_{m} versus 1/|δ0(T)1/|\delta_{0}(T). The NiAl data show a downward deviation towards T=MsT=M_{s} marked by the downward arrow.Using the extracted B0B_{0} values, the intercepts are found in a fit to y=B0x+y0y=B_{0}x+y_{0}.
Refer to caption
Figure 21: Entropy barrier collapse and divergence in scaled variables, for experiment: Combined data from experiments in linear-linear plot of log(t/t0)\log(t/t_{0}) versus B/|δ0(T)|B/|\delta_{0}(T)|. The dashed straight line is the universal Vogel-Fulcher-Tammann form of the diverging entropy barrier. Some data show a downward turn for entropy barrier collapse.

Fig 21 shows that combined experimental data R16 ; R17 ; R18 cluster around the Vogel-Fulcher straight line of Equ (30), with universality over 3 orders of magnitude near TdT_{d}. For NiAl dataR18 , there is a linear falloff on approaching T1T_{1} (downward arrow), consistent with Fig 16.

It would be interesting to get more data for these and other martensitic alloys, through systematic quenches in steps of 1/|δ0(T)|1/|\delta_{0}(T)|, over the entire delay range Ms<T<TdM_{s}<T<T_{d} between barrier divergence and collapse. It would also be interesting to include a T1T_{1}-like onset of sluggishness, in fitting analyses of glass-former viscosity data R7

VIII Summary and further work

In this paper, we present Monte Carlo (MC) simulations, on discrete-strain Hamiltonians for four 3D structural transitions, under systematic temperature quenches from seeded austenite, to study austenite-to-martensite conversion times. The results and scenario are as follows.

For athermal martensites, there are explosive conversions below a martensite start temperature MsM_{s} so there are no barriers. Above this start temperature, entropy barriers emerge , and incubation time delays rise sharply towards a divergence temperature TdT_{d}. The entropy barrier collapse/ divergence, is understood through temperature-controlled phase-space bottlenecks.

Partial equilibration ideas provide an understanding of fast/ slow times, based on effective temperatures for energy-lowering searches. The inverse search temperature vanishes linearly at MsM_{s} or 1/Teff(T)|TMs|01/T_{eff}(T)\sim|T-M_{s}|\rightarrow 0. The search temperature vanishes linearly at TdT_{d}, or Teff(T)|TTd|0T_{eff}(T)\sim|T-T_{d}|\rightarrow 0. This rapid search arrest explains the singular Vogel-Fulcher-Tammann form, extracted from martensitic experimental data.

Further simulations of crystallisation models R6 could try to record heat releases. Further experiments could record strain signals and intermittencyR40 over the delay region Td>T>T1T_{d}>T>T_{1}; and over the tweed precursor R14 ; R25 ; R27 region above it T0>T>TdT_{0}>T>T_{d}. Non-stationary distributions of energy changes in martensites could be measured through concurrent acoustic, photonic or strain probesR40 . The VFT temperature regime in glasses shows non-Debye frequency responses R9 : this might be more general. Finally, quenches of complex oxides R41 near their structural / functional transitions, might yield interesting PES signatures in functional variables, induced by their coupling to ageing strain domains.

Acknowledgements:
It is a pleasure to thank Turab Lookman for helpful early conversations; and Smarajit Karmakar for valuable discussions on the glass transition.

Appendix A: PES signatures in the m4m^{4} model:

As a toy model illustration of the Section III procedure we consider a 2D magnetization free energy with double-well Landau term and a Ginzburg term, F=E0r[fL+fG]F=E_{0}\sum_{\vec{r}}[f_{L}+f_{G}], Here mm is the single component OP, of both signs, so NOP=1,NV=2N_{OP}=1,N_{V}=2. The Landau term is

fL(m(r))=ϵ(T)m(r)2+m(r)4/2f_{L}(m(\vec{r}))~{}=\epsilon(T)m(\vec{r})^{2}+{m(\vec{r})^{4}}/2 (31)

where ϵ(T)(TTc)/Tc\epsilon(T)\equiv(T-T_{c})/T_{c}, with all energies/ temperatures scaled in the physical transition temperature, so the scaled Tc=1T_{c}=1. The Ginzburg term is fG=ξ02[Δm(r)2]f_{G}=\xi_{0}^{2}[{{\Delta m}(\vec{r})}^{2}].

Refer to caption
Figure 22: Magnetization fraction and PES distribution:   a) Linear-linear plot of magnetization fraction nm(t)n_{m}(t) versus time after a quench to T=0.5T=0.5. The curve at nm(tm)=1/2n_{m}(t_{m})=1/2 defines a halfway time tm(T)t_{m}(T), that here is tm=107t_{m}=107 MC steps.   b) Log-linear histogram of normalized probability of heat release P0(δE,T)P_{0}(\delta E,T) versus δE\delta E after the quench, recording energy changes up to waiting times tw=tm(T)t_{w}=t_{m}(T). Here the slope is βeff/2=0.09\beta_{eff}/2=0.09, or Teff=5.6T_{eff}=5.6.

.

Domain-walls are solitonic solutions with a tanh\tanh profile, interpolating between flat OP variants of opposite sign, within a DW thickness ξ01\xi_{0}\sim 1. The OP can be written as a magnitude |m||m| times a variant ‘spin’ S(r)=±1S(\vec{r})=\pm 1 of unit length. The nearly flat magnitude in the domains is approximated by the mean field OP,

m(r)|m(r)|S(r)m¯(T)S(r)m(\vec{r})\equiv|m(\vec{r})|S(\vec{r})\rightarrow{\bar{m}}(T)S(\vec{r}) (32)

where m¯(T)=|ϵ(T)|1/2{\bar{m}}(T)=|\epsilon(T)|^{1/2}. Compare Equ (7).

The mean-field Landau free energy is

fL(T)=m¯(T)2gL(T);gL=12|ϵ(T)|<0.f_{L}(T)={\bar{m}}(T)^{2}g_{L}(T);~{}g_{L}=-\frac{1}{2}|\epsilon(T)|<0. (33)

where gL(Tc)=0g_{L}(T_{c})=0. Compare Equ (10).

Substituting Equ (32) in Equ (31) yields the DW coordinate space Hamiltonian, with D02m¯2E0/TD_{0}\equiv 2{\bar{m}}^{2}E_{0}/T,

βH=(D0/2)r[|gL(T)|S(r)2+ξ02(ΔS(r))2],\beta H=(D_{0}/2)\sum_{\vec{r}}[-|g_{L}(T)|S(\vec{r})^{2}+\xi_{0}^{2}(\Delta S(\vec{r}))^{2}], (34)

although in this case, S(r)2=1S(\vec{r})^{2}=1 at all sites. With S(r)=keik.rS(k)/NS(\vec{r})=\sum_{\vec{k}}e^{i\vec{k}.\vec{r}}S(\vec{k})/\sqrt{N}, the Hamiltonian in Fourier space is

βH=(D0/2)k[|gL(T)|+ξ02K(k)2]|S(k)|2.\beta H=(D_{0}/2)\sum_{\vec{k}}[-|g_{L}(T)|+\xi_{0}^{2}{\vec{K}}(\vec{k})^{2}]|S(\vec{k})|^{2}. (35)

Compare Equ (13) and Equ (14).

We can do MC simulations with this T-dependent, Ising-variant effective Hamiltonian. The parameters are N=642,ξ02=1,Nrun=10N=64^{2},\xi_{0}^{2}=1,N_{run}=10, with holding times th=103t_{h}=10^{3}. The spin-flips are S=±11S=\pm 1\rightarrow\mp 1. Fig 22a shows the magnetization fraction nm(t)n_{m}(t) versus waiting time twt_{w} analogous to Fig 3, but here with a gradual rise, and no incubation behaviour.

We record {δE}\{\delta E\} for every spin flip up to an OP marker event time tw=tmt_{w}=t_{m} when nm(tm)=1/2n_{m}(t_{m})=1/2. For nearest-neighbour couplings on a square lattice, the energy changes δE\delta E will be discrete. Fig 22b shows the log-linear P0(δE,tw=tm)P_{0}(\delta E,t_{w}=t_{m}) versus discrete energy changes δE\delta E. The spike heights decrease linearly with energy changes, consistent with PES. Compare Fig 15.

Refer to caption
Figure 23: Tetragonal-orthorhombic TTT curve, showing both explosive and incubated conversions: Figures show TTT curves as log-linear plots of time versus quench temperature. Flat regions along the x-axis denote single time-step conversions up to end points T=T1T=T_{1}, defining athermal regime materials. The T1T_{1} depend on the elastic constants A1A_{1} and spinodal temperatures TcT_{c}. For some parameters, T1T_{1} is driven to zero, and the TTT curves intersect the y-axis. These materials are in a ‘mixed’ regime. See text.

Appendix B: Athermal phase diagram:

Refer to caption
Figure 24: Phase diagrams for athermal/ mixed behaviour: Four-panel Figure showing linear-linear plots of TcT_{c} versus A1A_{1} solid line the theoretical boundary between athermal and mixed materials. Simulation data for athermal (open circles) and mixed (open squares) behaviour, are consistent with the theoretical curve.

Fig 23 shows data for the martensitic tetragonal-orthorhombic transition, for several Tc,A1T_{c},A_{1}, showing both athermal and non-athermal or mixed behaviour R11 ; R23 ; R24 ; R25 . For the athermal regime, Temperature-Time-Transformation (TTT) curves have flat lines along the temperature axis where there are immediate, explosive conversions for T<T1T<T_{1}. The embryo or droplet is small in coordinate space, and so is broad and flat in Fourier space. With |S(k)|2|{\vec{S}}(\vec{k})|^{2} approximated by a constant, the Hamiltonian energy of Equ (18) is E/D0kϵ(k)E/D_{0}\sim\sum_{\vec{k}}\epsilon(\vec{k}) then involves averages of terms over the Brillouin Zone, denoted by square brackets. The droplet energy is

E(T)/D0|gL(T)|+{ξ02[K2(k)]+(A1/2)[U,(k^)]}.E(T)/D_{0}\simeq-|g_{L}(T)|+\{\xi_{0}^{2}[K^{2}(\vec{k})]+(A_{1}/2)[U_{\ell,\ell}(\hat{k})]\}. (36)

The energy vanishing E(T1)=0E(T_{1})=0 defines T=T1T=T_{1}. For small values in a Taylor expansion, and with coefficient b(T)b(T) as defined in the text,

T1(A1,Tc){+|gL(0)|ξ02[K2(k)](A1/2)[U,(k^)]}/|b(0)|.T_{1}(A_{1},T_{c})\simeq\{+|g_{L}(0)|-\xi_{0}^{2}[K^{2}(\vec{k})]-(A_{1}/2)[U_{\ell,\ell}(\hat{k})]\}/|b(0)|. (37)

We define ‘athermal’ behaviour as a nonzero T1T_{1}; explosive conversions for T<T1T<T_{1}; and incubation delays in the window T1<T<Td<T0T_{1}<T<T_{d}<T_{0}. The behaviour not precisely athermal, is called ‘mixed’, with conversions occurring gradually, without flat incubations. Vanishing of the athermal case start temperature T1(A1,Tc)=0T_{1}(A_{1},T_{c})=0 then determines a phase boundary.

The four-panel Fig 24 plot of TcT_{c} versus A1A_{1}, shows the phase boundary. Above the phase boundary the system is purely athermal, while below the phase boundary where T1=0T_{1}=0, is a mixed regime. Data from Fig 23 and other TTT diagrams are seen to be consistent with the theoretical phase boundary. Fig 23 shows that for some parameters, curves on the upper left, have a fall and then a rise with temperature, like a ‘U shape, or downward ‘nose’ . For the large E0=3E_{0}=3 used, the shape is distorted, but for smaller E0<1E_{0}<1 the U shape is more well defined R26 . The shape is from an Arrhenius activation over a temperature-dependent energy barrierR42 .

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