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  <front>
    <journal-meta>
      <journal-id journal-id-type="nlm-ta">J. Mater. Inf.</journal-id>
      <journal-id journal-id-type="publisher-id">JMI</journal-id>
      <journal-title-group>
        <journal-title>Journal of Materials Informatics</journal-title>
      </journal-title-group>
      <issn pub-type="epub">2770-372X</issn>
      <publisher>
        <publisher-name>OAE Publishing Inc.</publisher-name>
      </publisher>
    </journal-meta>
    <article-meta>
      <article-id pub-id-type="doi">10.20517/jmi.2026.05</article-id>
      <article-categories>
        <subj-group>
          <subject>Research Article</subject>
        </subj-group>
      </article-categories>
      <title-group>
        <article-title>Phase Lab: a cloud-native CALPHAD-to-data platform for accelerated alloy design and AI/ICME/MGE workflows</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes">
          <name>
            <surname>Yan</surname>
            <given-names>Lihui</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
          <xref ref-type="aff" rid="I*">
            <sup>*</sup>
          </xref>
          <xref ref-type="corresp" rid="cor1" />
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Wu</surname>
            <given-names>Qiaojun</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Chen</surname>
            <given-names>Yikai</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Dong</surname>
            <given-names>Rui</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Zhang</surname>
            <given-names>Weijie</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
        </contrib>
        <contrib contrib-type="author" corresp="yes">
          <name>
            <surname>Gong</surname>
            <given-names>Kui</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
          <xref ref-type="aff" rid="I*">
            <sup>*</sup>
          </xref>
          <xref ref-type="corresp" rid="cor1" />
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Liu</surname>
            <given-names>Xingjun</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
          <xref ref-type="aff" rid="I2">
            <sup>2</sup>
          </xref>
        </contrib>
        <contrib contrib-type="author">
          <name>
            <surname>Wang</surname>
            <given-names>Yin</given-names>
          </name>
          <xref ref-type="aff" rid="I1">
            <sup>1</sup>
          </xref>
        </contrib>
      </contrib-group>
      <aff id="I1">
        <sup>1</sup>Hongzhiwei Technology (Shanghai) Co., Ltd., Shanghai 200120, China.</aff>
      <aff id="I2">
        <sup>2</sup>School of Materials Science and Engineering and Institute of Materials Genome and Big Data, Harbin Institute of Technology, Shenzhen 518055, Guangdong, China.</aff>
      <author-notes>
        <corresp id="cor1"><sup>*</sup>Correspondence to: Lihui Yan, Kui Gong, Hongzhiwei Technology (Shanghai) Co., Ltd., Shanghai 200120, China. E-mail: <email>yanlihui@hzwtech.com</email>; <email>gongkui@hzwtech.com</email></corresp>
        <fn fn-type="other">
          <p>
            <bold>Received:</bold> 14 Feb 2026 | <bold>First Decision:</bold> 9 Apr 2026 | <bold>Revised:</bold> 30 Apr 2026 | <bold>Accepted:</bold> 19 May 2026 | <bold>Published:</bold> 28 May 2026</p>
        </fn>
        <fn fn-type="other">
          <p>
            <bold>Academic Editor:</bold> Yong Du | <bold>Copy Editor:</bold> Pei-Yun Wang | <bold>Production Editor:</bold> Pei-Yun Wang</p>
        </fn>
      </author-notes>
      <pub-date pub-type="ppub">
        <year>2026</year>
      </pub-date>
      <pub-date pub-type="epub">
        <day>28</day>
        <month>5</month>
        <year>2026</year>
      </pub-date>
      <volume>6</volume>
	  <issue>2</issue>
      <elocation-id>33</elocation-id>
      <permissions>
        <copyright-statement>© The Author(s) 2026.</copyright-statement>
        <license xlink:href="https://creativecommons.org/licenses/by/4.0/">
          <license-p>© The Author(s) 2026. <bold>Open Access</bold> This article is licensed under a Creative Commons Attribution 4.0 International License (<uri xlink:href="https://creativecommons.org/licenses/by/4.0/">https://creativecommons.org/licenses/by/4.0/</uri>), which permits unrestricted use, sharing, adaptation, distribution and reproduction in any medium or format, for any purpose, even commercially, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.</license-p>
        </license>
      </permissions>
      <abstract>
        <p>Artificial intelligence (AI)-assisted alloy design, integrated computational materials engineering (ICME), and materials genome engineering (MGE) increasingly require CALculation of PHAse Diagrams (CALPHAD) calculations to be executed at scale and stored as reusable, traceable data. However, conventional CALPHAD workflows are often desktop-centered and tool-specific, which limits reproducibility, high-throughput reuse, and direct integration with machine-learning pipelines. Here we present Phase Lab, a cloud-native CALPHAD-to-data platform designed for alloy designers, CALPHAD practitioners, and AI/ICME/MGE researchers who require scalable computation together with standardized data products. Rather than introducing new physical models, Phase Lab standardizes the full calculation workflow, including browser-based configuration, application programming interface-driven task orchestration, server-side computation, metadata capture, provenance tracking, and structured export. The platform supports thermodynamic, kinetic, thermophysical, solidification, and mechanical-property calculations, while storing database versions, model selections, input conditions, solver settings, and execution records. Point-to-point benchmark calculations showed agreement with Thermo-Calc for representative ternary systems, and batch tests achieved a 100% completion rate for 20,000 ternary tasks with an average runtime of 0.006933 s per task. For 9-component and 12-component systems, completion rates of 99.32% and 98.14% were obtained, respectively, with average runtimes of 1.122 and 2.19 s per task. Validation against literature and experimental data across Fe-, Ni-, Al-, and Cu-based systems further demonstrated the applicability of the platform. For Ni-based superalloys, the room-temperature yield-strength and ultimate-tensile-strength models achieved <italic>R</italic><sup>2</sup> values of 0.858 and 0.824, respectively. These results indicate that Phase Lab can serve as a practical data-generation platform for dataset assembly, surrogate modeling, active learning, and ICME/MGE-oriented alloy screening.</p>
      </abstract>
      <kwd-group>
        <kwd>Cloud-native platform</kwd>
        <kwd>CALPHAD</kwd>
        <kwd>ICME</kwd>
        <kwd>MGE</kwd>
        <kwd>AI</kwd>
        <kwd>alloy design</kwd>
      </kwd-group>
    </article-meta>
  </front>
  <body>
    <sec id="sec1">
      <title>INTRODUCTION</title>
      <p>Thermodynamic and kinetic modeling based on CALculation of PHAse Diagrams (CALPHAD) provides a physically grounded foundation for alloy design, process optimization, and microstructure control. It has become a routine component of integrated computational materials engineering (ICME)<sup>[<xref ref-type="bibr" rid="B1">1</xref>-<xref ref-type="bibr" rid="B8">8</xref>]</sup> in both industrial practice and academic research. More broadly, CALPHAD-based methods and related computational tools have been widely used in materials modeling studies for phase equilibria, solidification, diffusion, precipitation, thermophysical-property prediction, and composition/process screening across diverse alloy systems<sup>[<xref ref-type="bibr" rid="B2">2</xref>,<xref ref-type="bibr" rid="B9">9</xref>-<xref ref-type="bibr" rid="B14">14</xref>]</sup>. At the same time, emerging materials genome engineering (MGE) and artificial intelligence (AI)-driven strategies increasingly depend on large, consistent, and well-described datasets that can be aggregated, queried, and reused across alloy systems and projects<sup>[<xref ref-type="bibr" rid="B1">1</xref>,<xref ref-type="bibr" rid="B15">15</xref>-<xref ref-type="bibr" rid="B18">18</xref>]</sup>. A persistent bottleneck is that conventional CALPHAD packages such as Thermo-Calc<sup>[<xref ref-type="bibr" rid="B19">19</xref>]</sup>, PANDAT<sup>[<xref ref-type="bibr" rid="B20">20</xref>]</sup>, and JMatPro<sup>[<xref ref-type="bibr" rid="B21">21</xref>]</sup> are still often executed as isolated, desktop-centered tasks: computations are not easily scaled to high-throughput screening, and the resulting outputs are frequently stored as ad hoc logs or figures with incomplete provenance, limiting reproducibility and direct reuse in AI/ICME/MGE pipelines. At a more fundamental level, CALPHAD results are still commonly generated in a tool-specific and case-by-case manner, making them difficult to reproduce, compare, aggregate, and directly reuse as structured data in ICME and AI-assisted alloy design workflows. To address these limitations, we developed Phase Lab as a cloud-native CALPHAD-to-data platform. The aim is not to replace established thermodynamic or kinetic formalisms, but to standardize how CALPHAD calculations are configured, executed, recorded, and exported. Phase Lab combines browser-based interaction, application programming interface (API)-driven task orchestration, server-side high-performance computing (HPC) computation, metadata capture, provenance tracking, and structured data export within a single workflow. As summarized in <xref ref-type="fig" rid="fig1">Figure 1</xref>, the platform shifts CALPHAD practice from fragmented, tool-specific calculations toward reusable data products that can be directly connected to AI, machine learning (ML), ICME, MGE, and optimization workflows.</p>
      <fig id="fig1" position="float">
        <label>Figure 1</label>
        <caption>
          <p>Phase Lab workflow from CALPHAD computation to reusable data products. Phase Lab converts conventional CALPHAD calculations into structured data products through browser-based configuration, API-driven orchestration, server-side CALPHAD/HPC execution, metadata management, provenance tracking, and database/model versioning. The resulting CSV, JSON, API/schema, and metadata-linked database records can be reused in AI/ML, ICME, MGE, and optimization workflows. CALPHAD: CALculation of PHAse Diagrams; API: application programming interface; HPC: high-performance computing; CSV: comma-separated values; JSON: JavaScript Object Notation; AI: artificial intelligence; ML: machine learning; ICME: integrated computational materials engineering; MGE: materials genome engineering.</p>
        </caption>
        <graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="jmi6005.fig.1.jpg" />
      </fig>
    </sec>
    <sec id="sec2">
      <title>MATERIALS AND METHODS</title>
      <sec id="sec2-1">
        <title>Physical models</title>
        <p>Phase Lab is built on established CALPHAD methodology and provides a thermodynamically consistent framework for multicomponent alloy calculations. Its main contribution is not the introduction of new physical models, but the integration of thermodynamic, kinetic, thermophysical, solidification, and mechanical-property calculations within a reproducible computational workflow. Thermodynamic modules determine phase stability, phase fractions, phase compositions, and thermodynamic driving forces. Kinetic modules describe time-dependent composition and microstructural evolution under prescribed thermal or processing histories. Property modules use the resulting thermodynamic and microstructural descriptors to estimate thermophysical and mechanical properties. This shared-state design helps maintain consistency across composition–process–microstructure–property calculations. To support technologically relevant alloys (Ni-, Fe-, Al-, Cu-, Ti-, and Mg-based systems), the platform integrates validated model families widely adopted in the CALPHAD community.</p>
        <p>In Phase Lab, thermodynamic parameters are specified for each phase according to the corresponding phase model and are obtained from the underlying thermodynamic database. Depending on the structural characteristics and compositional degrees of freedom of the phase, the corresponding description may range from stoichiometric models to multicomponent sublattice formulations. In practical CALPHAD assessments, many phase descriptions are represented within variants of the Compound Energy Formalism (CEF)<sup>[<xref ref-type="bibr" rid="B22">22</xref>]</sup>, which provides a general framework for describing gas phases, substitutional solutions, intermetallic compounds, ordered phases, and liquids exhibiting short-range order. The general equation for describing the Gibbs energy function per mole formula unit of a phase <italic>G<sub>M</sub><sup>a</sup></italic> is</p>
        <p><disp-formula> <label>(1)</label> <tex-math id="E1"> $$  G_{M}^{a}={ }^{srf}G_{M}^{a}+{ }^{cfg}G_{M}^{a}+{ }^{phy}G_{M}^{a}+{ }^{E}G_{M}^{a} $$ </tex-math></disp-formula></p>
        <p>where <italic><sup>srf</sup></italic><italic>G<sub>M</sub><sup>a</sup></italic> denotes the “surface” of reference for the phase relative to other phases and internal ordering; <italic><sup>cfg</sup></italic><italic>G<sub>M</sub><sup>a</sup></italic> is the configurational term which assumes ideal mixing of the constituents in each sublattice, <italic><sup>phy</sup></italic><italic>G<sub>M</sub><sup>a</sup></italic> is used to describe contributions to the Gibbs energy from particular physical phenomena like magnetic transitions, and <italic><sup>E</sup></italic><italic>G<sub>M</sub><sup>a</sup></italic> is needed to describe deviations in the Gibbs energy relative to the first three terms. Additional magnetic and ordering contributions are incorporated where required by the adopted phase model<sup>[<xref ref-type="bibr" rid="B23">23</xref>-<xref ref-type="bibr" rid="B26">26</xref>]</sup>.</p>
        <p>Based on Fick’s law, diffusion kinetics simulations predict time-dependent composition profiles within a diffusion couple<sup>[<xref ref-type="bibr" rid="B19">19</xref>,<xref ref-type="bibr" rid="B27">27</xref>]</sup>. The composition- and temperature-dependent diffusion coefficients are calculated using the atomic mobility parameters and thermodynamic factors. Precipitation kinetics is modeled using the Kampmann-Wagner Numerical (KWN) method, describing nucleation, growth, and coarsening behaviors over time and/or temperature variations<sup>[<xref ref-type="bibr" rid="B28">28</xref>]</sup>. Non-equilibrium solidification paths are modeled using the classical Scheil-Gulliver model and improved partial equilibrium approximations that consider rapid diffusion behavior of interstitial atoms<sup>[<xref ref-type="bibr" rid="B29">29</xref>,<xref ref-type="bibr" rid="B30">30</xref>]</sup>. Based on the resulting solidification paths, several hot cracking susceptibility criteria were evaluated within a unified framework. These criteria are derived from the temperature–solid fraction (<italic>T</italic>-<italic>fs</italic>) relationship during solidification and include the solidification interval (<italic>SI</italic>), the Clyne-Davies cracking susceptibility coefficient (<italic>CSC</italic>), the critical temperature interval (<italic>CTI</italic>), and Kou’s solidification cracking index (<italic>SCI</italic>), all of which are evaluated in a consistent framework<sup>[<xref ref-type="bibr" rid="B2">2</xref>,<xref ref-type="bibr" rid="B12">12</xref>,<xref ref-type="bibr" rid="B31">31</xref>]</sup>. They are described in detail as follows:</p>
        <p><disp-formula> <label>(2)</label> <tex-math id="E1"> $$  SI=T_L-T_{(fs=0.95)} $$ </tex-math></disp-formula></p>
		<p><disp-formula> <label>(3)</label> <tex-math id="E1"> $$  CSC=\frac{t_{fs=0.99}-t_{fs=0.90}}{t_{fs=0.90}-t_{fs=0.40}}\approx \frac{T_{fs=0.99}-T_{fs=0.90}}{T_{fs=0.90}-T_{fs=0.40}} $$ </tex-math></disp-formula></p>
		<p><disp-formula> <label>(4)</label> <tex-math id="E1"> $$  CTI=T_{(fs=0.7)}-T_{(fs=0.85)} $$ </tex-math></disp-formula></p>
		<p><disp-formula> <label>(5)</label> <tex-math id="E1"> $$  SCI=\left | \frac{dT}{dfs} \right | $$ </tex-math></disp-formula></p>
		<p>where <italic>T<sub>L</sub></italic> is the liquidus temperature and <italic>T</italic><sub>(<italic>fs</italic>)</sub> denotes the temperature corresponding to a given solid fraction <italic>fs</italic>. The terminal solidification temperature in the <italic>SI</italic> definition was approximated by <italic>T</italic><sub>(<italic>fs</italic>=0.95)</sub> to avoid overestimation of the freezing range in the high-fs regime of Scheil calculations. Under an approximately constant cooling rate, the time ratio in the <italic>CSC</italic> criterion can be equivalently expressed in terms of the corresponding temperature intervals. In this work, <italic>SCI</italic> was evaluated either as an average slope over a specified terminal solid-fraction interval or as a local slope near a selected solid fraction, depending on the specific comparison and reporting format. In general, larger values of <italic>SI</italic>, <italic>CSC</italic>, and <italic>SCI</italic> indicate higher hot cracking susceptibility.</p>
        <p>Beyond computational phase equilibrium and kinetic simulations, Phase Lab provides thermophysical and mechanical property modules. Thermophysical properties, such as molar volume<sup>[<xref ref-type="bibr" rid="B32">32</xref>,<xref ref-type="bibr" rid="B33">33</xref>]</sup>, density, viscosity<sup>[<xref ref-type="bibr" rid="B34">34</xref>,<xref ref-type="bibr" rid="B35">35</xref>]</sup>, and thermal/electrical conductivity<sup>[<xref ref-type="bibr" rid="B36">36</xref>-<xref ref-type="bibr" rid="B38">38</xref>]</sup>, are computed using CALPHAD-consistent formulations. In these models, the relevant properties are expressed as temperature- and composition-dependent functions of phase constitution and phase composition, with model parameters taken from the underlying property databases. The conductivity models are currently intended for metallic alloy systems and corresponding phases covered by the implemented parameter sets; their applicability therefore depends on the availability and assessed quality of the relevant thermodynamic/property descriptions for the target alloy system. Accordingly, the predicted thermal and electrical conductivities represent intrinsic phase-level behavior under the assumed composition-temperature conditions, and do not explicitly account for microstructural features such as porosity, texture, or defect scattering introduced by specific processing routes.</p>
        <p>Mechanical properties are evaluated using physically based strengthening models<sup>[<xref ref-type="bibr" rid="B39">39</xref>-<xref ref-type="bibr" rid="B42">42</xref>]</sup>. The yield strength (YS) is expressed as</p>
        <p><disp-formula> <label>(6)</label> <tex-math id="E1"> $$  \sigma_y=\sigma_0+\Delta \sigma_{ss}+\Delta \sigma_{HP}+\Delta \sigma_{ppt} $$ </tex-math></disp-formula></p>
        <p>where <italic>σ</italic><sub>0</sub> is the base strength, and Δ<italic>σ<sub>ss</sub></italic>, Δ<italic>σ<sub>HP</sub></italic>, Δ<italic>σ<sub>ppt</sub></italic> denote the contributions from solid-solution strengthening, grain-boundary strengthening, and precipitation strengthening, respectively. In the current implementation, precipitation strengthening is described through microstructural descriptors such as precipitate fraction and characteristic size, rather than explicit treatment of full precipitate morphology evolution. The present mechanical-property module is primarily intended for strength estimation under prescribed microstructural states; it does not explicitly resolve detailed dislocation evolution during deformation, and predictions of ultimate tensile strength (UTS) are therefore based on calibrated structure-property relationships within the supported alloy classes.</p>
        <p>At the present stage, Phase Lab is a CALPHAD-centered thermodynamic, kinetic, and property data platform rather than a full multiscale simulation engine. The current validation focuses mainly on metallic alloy systems, because the implemented thermodynamic, mobility, and property descriptions are primarily assessed for metallic phases. In principle, the CALPHAD-to-data workflow can be extended to non-metallic systems such as oxides, ceramics, and salts, provided that suitable databases and property models are available and validated. Direct execution of density functional theory (DFT), molecular dynamics (MD), phase-field, or finite-element simulations is not included, but API/schema-defined data objects allow CALPHAD-derived quantities to be exchanged with external multiscale workflows. The platform currently uses validated internal and version-controlled databases; user-defined database import is under development and will require compatibility checking and provenance registration before routine use.</p>
      </sec>
      <sec id="sec2-2">
        <title>Phase equilibrium algorithm</title>
        <p>Phase Lab computes multicomponent equilibrium by minimizing the total Gibbs free energy under mass-balance constraints following the approach of Sundman<sup>[<xref ref-type="bibr" rid="B25">25</xref>]</sup>. The total Gibbs energy (<italic>G</italic>) is written as:</p>
        <p><disp-formula> <label>(7)</label> <tex-math id="E1"> $$  G=\sum_aN^aG_M^a(T,P,Y) $$ </tex-math></disp-formula></p>
        <p>where <italic>N<sup>a</sup></italic> is the mole fraction of phase <italic>a</italic>, and <italic>G<sub>M</sub><sup>a</sup></italic> is the molar Gibbs energy of that phase as a function of temperature <italic>T</italic>, pressure <italic>P</italic>, and its constitution <italic>Y</italic>. The solver adopts a Lagrange multiplier formulation in which chemical potentials enforce mass balance. The procedure includes initialization by grid-based phase scanning<sup>[<xref ref-type="bibr" rid="B43">43</xref>,<xref ref-type="bibr" rid="B44">44</xref>]</sup>, iterative linearization to update phase amounts and compositions, and a dynamic stability check that activates dormant phases when their driving forces become positive, promoting convergence toward the global equilibrium solution. To generate phase diagrams and property maps efficiently, Phase Lab implements a Zero-Phase-Fraction (ZPF) tracking algorithm<sup>[<xref ref-type="bibr" rid="B45">45</xref>]</sup> and uses automated global search/backtracking to resolve complex topologies.</p>
      </sec>
      <sec id="sec2-3">
        <title>Computational workflow and information transmission</title>
        <p>The computational workflow of Phase Lab is organized as a CALPHAD-to-data pipeline, as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>. The pipeline standardizes the calculation lifecycle from user input to structured data export, including task submission, solver execution, result parsing, metadata attachment, provenance recording, persistent storage, and downstream reuse. The platform separates user interaction, application services, and numerical computation into three layers. The browser-based frontend supports module selection, parameter configuration, task submission, result visualization, and data export. The application layer provides user authentication, API services, input validation, solver-input generation, task orchestration, and centralized scheduling. The computational layer contains the server-side CALPHAD/HPC kernel, implemented mainly in C++ (over 70,000 lines of code), which performs Gibbs-energy minimization, diffusion and precipitation calculations, solidification simulations, and property evaluations using thermodynamic, kinetic, and property databases.</p>
        <p>A typical calculation starts from a user-defined request containing the alloy system, composition, target module, thermodynamic conditions, and optional processing history. The request is submitted through the frontend or API and translated by the application layer into solver-ready input files (e.g., PhaseLab.in). The task is then assigned to a server-side compute node through the scheduler. After execution, numerical outputs and log files (e.g., PhaseLab.log), are parsed and linked with the corresponding input conditions, database version, model selection, solver settings, timestamp, and execution record. The parsed results are returned to the frontend for visualization and export, while raw files, structured outputs, and provenance records are stored persistently.</p>
        <p>Each calculation is therefore represented not only as a numerical result, but also as a structured data object. Depending on the module, the exported data may include phase equilibria, phase fractions, phase compositions, transformation temperatures, diffusion profiles, precipitation descriptors, solidification curves, hot-cracking indices, thermophysical properties, or mechanical-property estimates. These outputs can be exported as comma-separated values (CSV) tables, JavaScript Object Notation (JSON) files, API/schema-defined records, or database objects linked to metadata and provenance. This representation allows CALPHAD results to be aggregated across alloy systems and reused in AI/ML, ICME, MGE, and optimization workflows without manual reconstruction of the calculation context.</p>
        <p>A representative point-calculation output can be stored as a structured JSON-like data object, in which the input conditions, thermodynamic quantities, stable phases, phase fractions, and phase compositions are linked within the same record:</p>
		<p>1&#xA0;{<break/>2&#xA0;&#xA0;&#xA0;"module": "Phase_diagram",<break/>3&#xA0;&#xA0;&#xA0;"task": "Point",<break/>4&#xA0;&#xA0;&#xA0;"alloy_system": "Al-Mg-Zn",<break/>5&#xA0;&#xA0;&#xA0;"composition": {<break/>6&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"unit": "mass_fraction",<break/>7&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Al": 0.77,<break/>8&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Mg": 0.10,<break/>9&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Zn": 0.13<break/>10&#xA0;&#xA0;},<break/>11&#xA0;&#xA0;"conditions": {<break/>12&#xA0;&#xA0;&#xA0;&#xA0;"temperature_K": 300,<break/>13&#xA0;&#xA0;&#xA0;&#xA0;"pressure_Pa": 101325,<break/>14&#xA0;&#xA0;&#xA0;&#xA0;"total_moles": 1<break/>15&#xA0;&#xA0;},<break/>16&#xA0;&#xA0;"thermodynamic_outputs": {<break/>17&#xA0;&#xA0;&#xA0;&#xA0;"gibbs_energy_J_per_mol": -10446.34,<break/>18&#xA0;&#xA0;&#xA0;&#xA0;"enthalpy_J_per_mol": -1174.60,<break/>19&#xA0;&#xA0;&#xA0;&#xA0;"entropy_J_per_mol_K": 30.9058,<break/>20&#xA0;&#xA0;&#xA0;&#xA0;"heat_capacity_J_per_mol_K": 25.0878<break/>21&#xA0;&#xA0;},<break/>22&#xA0;&#xA0;"system_composition": [<break/>23&#xA0;&#xA0;&#xA0;&#xA0;{<break/>24&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"component": "Al",<break/>25&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mole_fraction": 0.8238322,<break/>26&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mass_fraction": 0.7700000,<break/>27&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"chemical_potential": -8499.20,<break/>28&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"activity": 0.0331280<break/>29&#xA0;&#xA0;&#xA0;&#xA0;},<break/>30&#xA0;&#xA0;&#xA0;&#xA0;{<break/>31&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"component": "Mg",<break/>32&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mole_fraction": 0.1187754,<break/>33&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mass_fraction": 0.1000000,<break/>34&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"chemical_potential": -15643.61,<break/>35&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"activity": 0.0018892<break/>36&#xA0;&#xA0;&#xA0;&#xA0;},<break/>37&#xA0;&#xA0;&#xA0;&#xA0;{<break/>38&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"component": "Zn",<break/>39&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mole_fraction": 0.0573924,<break/>40&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mass_fraction": 0.1300000,<break/>41&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"chemical_potential": -27640.41,<break/>42&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"activity": 0.0000154<break/>43&#xA0;&#xA0;&#xA0;&#xA0;}<break/>44&#xA0;&#xA0;],<break/>45&#xA0;&#xA0;"phase_summary": {<break/>46&#xA0;&#xA0;&#xA0;&#xA0;"total_phases_considered": 34,<break/>47&#xA0;&#xA0;&#xA0;&#xA0;"number_of_stable_phases": 2,<break/>48&#xA0;&#xA0;&#xA0;&#xA0;"stable_phases": ["FCC_A1", "T_PHASE"]<break/>49&#xA0;&#xA0;},<break/>50&#xA0;&#xA0;"stable_phase_outputs": [<break/>51&#xA0;&#xA0;&#xA0;&#xA0;{<break/>52&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"phase": "FCC_A1",<break/>53&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mole_fraction": 0.7040631,<break/>54&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mass_fraction": 0.6578289,<break/>55&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"phase_composition": {<break/>56&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"unit": "mole_fraction",<break/>57&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Al": 0.9963126,<break/>58&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Mg": 0.0036748,<break/>59&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Zn": 0.0000126<break/>60&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;}<break/>61&#xA0;&#xA0;&#xA0;&#xA0;},<break/>62&#xA0;&#xA0;&#xA0;&#xA0;{<break/>63&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"phase": "T_PHASE",<break/>64&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mole_fraction": 0.2959369,<break/>65&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"mass_fraction": 0.3421711,<break/>66&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"phase_composition": {<break/>67&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"unit": "mole_fraction",<break/>68&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Al": 0.4134844,<break/>69&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Mg": 0.3926111,<break/>70&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;"Zn": 0.1939045<break/>71&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;&#xA0;}<break/>72&#xA0;&#xA0;&#xA0;&#xA0;}<break/>73&#xA0;&#xA0;],<break/>74&#xA0;&#xA0;"additional_outputs": "..."<break/>75}</p>
        <p>For time-temperature-transformation (TTT)/continuous-cooling-transformation (CCT) calculations, transformation-boundary points are stored as discrete temperature-time pairs at specified transformed fractions. Here, 0.1% and 99.9% transformation are used as representative start and finish criteria, respectively. Each record contains the diagram type, transformation product, criterion, temperature, and time. For CCT calculations, cooling paths are stored separately using cooling rate, temperature, and time. The exported records are direct solver outputs converted into standardized CSV or JSON/API formats; unless otherwise stated, no additional smoothing or empirical correction is applied. Representative long-format export fields generated by Phase Lab for TTT/CCT calculations are summarized in <xref ref-type="table" rid="t1">Table 1</xref>.</p>
        <table-wrap id="t1">
          <label>Table 1</label>
          <caption>
            <p>Representative long-format TTT/CCT export fields generated by Phase Lab</p>
          </caption>
          <table frame="hsides" rules="groups" pdfpage="9">
            <thead>
              <tr>
                <td style="border-bottom:1;">
                  <bold>Diagram type</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Product</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Criterion percent (%)</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Temperature (K)</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Time (s)</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Cooling rate (K/s)</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Data type</bold>
                </td>
              </tr>
            </thead>
            <tbody>
              <tr>
                <td>TTT</td>
                <td>Ferrite</td>
                <td>0.1</td>
                <td>801.15</td>
                <td>0.038</td>
                <td>N/A</td>
                <td>Boundary_point</td>
              </tr>
              <tr>
                <td>TTT</td>
                <td>Pearlite</td>
                <td>0.1</td>
                <td>801.15</td>
                <td>0.017</td>
                <td>N/A</td>
                <td>Boundary_point</td>
              </tr>
              <tr>
                <td>TTT</td>
                <td>Bainite</td>
                <td>99.9</td>
                <td>411.15</td>
                <td>244,675.394</td>
                <td>N/A</td>
                <td>Boundary_point</td>
              </tr>
              <tr>
                <td>CCT</td>
                <td>Ferrite</td>
                <td>0.1</td>
                <td>1,065.15</td>
                <td>822,751.000</td>
                <td>N/A</td>
                <td>Boundary_point</td>
              </tr>
              <tr>
                <td>CCT</td>
                <td>Bainite</td>
                <td>0.1</td>
                <td>800.15</td>
                <td>3,472,751.000</td>
                <td>N/A</td>
                <td>Boundary_point</td>
              </tr>
              <tr>
                <td>CCT</td>
                <td>Cooling path</td>
                <td>N/A</td>
                <td>1,147.43</td>
                <td>0.000</td>
                <td>0.1</td>
                <td>Cooling_path</td>
              </tr>
              <tr>
                <td>CCT</td>
                <td>Cooling path</td>
                <td>N/A</td>
                <td>1,142.43</td>
                <td>0.500</td>
                <td>10.0</td>
                <td>Cooling_path</td>
              </tr>
            </tbody>
          </table>
          <table-wrap-foot>
            <fn>
              <p>Note: N/A indicates that the field is not applicable. Cooling path records are stored separately from transformation-boundary records. TTT: Time-temperature-transformation; CCT: continuous-cooling-transformation.</p>
            </fn>
          </table-wrap-foot>
        </table-wrap>
        <p>This standardized data layer supports three common downstream uses. First, it enables AI/ML workflows such as dataset assembly, surrogate modeling, and active-learning export. Second, it supports ICME workflows for multi-objective screening and optimization under consistent provenance. Third, it allows MGE-oriented aggregation of computational property data across alloy systems. In this way, Phase Lab connects physics-based CALPHAD calculations with data-driven alloy design.</p>
      </sec>
    </sec>
    <sec id="sec3">
      <title>RESULTS AND DISCUSSION</title>
      <p>This section assesses the platform with respect to calculation accuracy, computational efficiency and stability, and agreement with literature and experimental data across different modules. The evaluation includes comparison with Thermo-Calc for representative ternary systems, stability tests for multicomponent batch calculations, and validation of phase equilibria, diffusion and atomic mobility, thermophysical properties, precipitation and phase transformation kinetics, mechanical performance, and solidification-related hot cracking susceptibility. Collectively, these results demonstrate the capability of the platform to generate reusable, provenance-rich CALPHAD data products for AI/ICME/MGE workflows.</p>
      <sec id="sec3-1">
        <title>Benchmark validation of thermodynamic calculations</title>
        <p>First, representative ternary systems were selected for direct comparison with Thermo-Calc in order to assess the accuracy and computational efficiency of the thermodynamic calculations. Owing to the functional and task-scale limitations of the Thermo-Calc 2025B (Free Educational Package version), the comparison was restricted to executable ternary calculations within its license scope. For each selected composition, molar Gibbs energy, liquidus temperature, and solidus temperature were calculated and compared under the same alloy system, composition, and calculation settings aligned as closely as practicable, including the thermodynamic database wherever applicable. In parallel, the average runtime per task and task completion rate were recorded for both codes in order to evaluate computational efficiency and execution stability.</p>
        <p>Representative comparisons of molar Gibbs energy, liquidus temperature, and solidus temperature are listed in <xref ref-type="table" rid="t2">Table 2</xref>. For the ten ternary benchmark cases, the values calculated by Phase Lab were the same as those obtained from Thermo-Calc for all three reported quantities. Specifically, the molar Gibbs energy values ranged from -22,296.34 to -10,446.34 J·mol<sup>-1</sup> in both codes, the liquidus temperatures ranged from 853.1618 to 1,604.5926 K, and the solidus temperatures ranged from 740.9668 to 937.7879 K. No numerical discrepancy was observed for the reported values in these benchmark examples.</p>
        <table-wrap id="t2">
          <label>Table 2</label>
          <caption>
            <p>Comparison of molar Gibbs energy at 300 K and calculated liquidus/solidus temperatures between Phase Lab and Thermo-Calc for representative ternary systems</p>
          </caption>
          <table frame="hsides" rules="groups" pdfpage="9">
            <thead>
              <tr>
                <td rowspan="2">
                  <bold>Composition (wt.%)</bold>
                </td>
                <td colspan="2">
                  <bold>Molar Gibbs energy at 300 K (J·mol<sup>-1</sup>)</bold>
                </td>
                <td colspan="2">
                  <bold>Liquidus temperature (K)</bold>
                </td>
                <td colspan="2">
                  <bold>Solidus temperature (K)</bold>
                </td>
              </tr>
              <tr>
                <td style="border-bottom:1;">
                  <bold>Thermo-Calc</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Phase Lab</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Thermo-Calc</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Phase Lab</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Thermo-Calc</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Phase Lab</bold>
                </td>
              </tr>
            </thead>
            <tbody>
              <tr>
                <td>80Al-10Cu-10Mg</td>
                <td>-12,217.67</td>
                <td>-12,217.67</td>
                <td>853.1618</td>
                <td>853.1618</td>
                <td>752.6879</td>
                <td>752.6879</td>
              </tr>
              <tr>
                <td>85Al-8Sc-7Ti</td>
                <td>-22,296.34 </td>
                <td>-22,296.34 </td>
                <td>1,481.1097</td>
                <td>1,481.1097</td>
                <td>937.7879</td>
                <td>937.7879</td>
              </tr>
              <tr>
                <td>78Al-12Zn-10Zr</td>
                <td>-15,130.86</td>
                <td>-15,130.86</td>
                <td>1,489.9027</td>
                <td>1,489.9027</td>
                <td>875.0246</td>
                <td>875.0246</td>
              </tr>
              <tr>
                <td>82Al-9Mg-9Sc</td>
                <td>-17,825.30</td>
                <td>-17,825.30</td>
                <td>1,307.4834</td>
                <td>1,307.4834</td>
                <td>757.1124</td>
                <td>757.1124</td>
              </tr>
              <tr>
                <td>75Al-15Cu-10Zr</td>
                <td>-18,590.74</td>
                <td>-18,590.74</td>
                <td>1,303.8679</td>
                <td>1,303.8679</td>
                <td>818.1481</td>
                <td>818.1481</td>
              </tr>
              <tr>
                <td>88Al-6Ti-6Zn</td>
                <td>-13,701.81</td>
                <td>-13,701.81</td>
                <td>1,381.1532</td>
                <td>1,381.1532</td>
                <td>911.7849</td>
                <td>911.7849</td>
              </tr>
              <tr>
                <td>79Al-11Mg-10Zr</td>
                <td>-15,160.33</td>
                <td>-15,160.33</td>
                <td>1,604.5926</td>
                <td>1,604.5926</td>
                <td>740.9668</td>
                <td>740.9668</td>
              </tr>
              <tr>
                <td>83Al-7Cu-10Ti</td>
                <td>-18,449.08</td>
                <td>-18,449.08</td>
                <td>1,479.1911</td>
                <td>1,479.1911</td>
                <td>821.6868</td>
                <td>821.6868</td>
              </tr>
              <tr>
                <td>86Al-8Sc-6Zn</td>
                <td>-16,663.20</td>
                <td>-16,663.20</td>
                <td>1,235.4275</td>
                <td>1,235.4275</td>
                <td>903.5287</td>
                <td>903.5287</td>
              </tr>
              <tr>
                <td>77Al-13Zn-10Mg</td>
                <td>-10,446.34</td>
                <td>-10,446.34</td>
                <td>858.2690</td>
                <td>858.2690</td>
                <td>741.5542</td>
                <td>741.5542</td>
              </tr>
            </tbody>
          </table>
          <table-wrap-foot>
            <fn>
              <p>Note: Only representative ternary compositions are listed here. All calculations were performed under matched system definitions and aligned calculation settings wherever practicable. Compositions are given in wt.%, and temperatures are reported in K.</p>
            </fn>
          </table-wrap-foot>
        </table-wrap>
        <p>The corresponding computational performance statistics are summarized in <xref ref-type="table" rid="t3">Table 3</xref>. In the ternary batch test, both Thermo-Calc and Phase Lab produced 20,000 valid outputs from 20,000 submitted tasks, corresponding to a completion rate of 100% for both codes. The average runtime per task was 0.011268 s for Thermo-Calc and 0.006933 s for Phase Lab under the present benchmark setting. These results indicate that Phase Lab reproduces the thermodynamic outputs of Thermo-Calc for the tested ternary systems while showing a shorter average runtime in this benchmark. Based on the ternary comparison, the assessment was further extended to multicomponent systems in order to evaluate computational efficiency and execution stability in higher-dimensional composition spaces. In this part, composition sets with different numbers of components were tested through batch execution under a unified calculation workflow. For the 9-component system, Phase Lab produced 9,932 valid outputs from 10,000 submitted tasks, corresponding to a completion rate of 99.32%, with an average runtime of 1.122 s per task. For the 12-component system, Phase Lab produced 9,814 valid outputs from 10,000 submitted tasks, corresponding to a completion rate of 98.14%, with an average runtime of 2.19 s per task. Equivalent multicomponent batch testing was not performed with Thermo-Calc because this was not supported by the Free Educational Package version used in this study. Overall, the results show that the platform maintains stable execution behavior under multicomponent batch-calculation conditions, while the average runtime increases with compositional dimensionality as expected.</p>
        <table-wrap id="t3">
          <label>Table 3</label>
          <caption>
            <p>Summary of computational performance and execution stability for Phase Lab and Thermo-Calc in ternary and multicomponent calculations</p>
          </caption>
          <table frame="hsides" rules="groups" pdfpage="10">
            <thead>
              <tr>
                <td style="border-bottom:1;">
                  <bold>System</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Code</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Number of tasks</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Valid outputs</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Completion rate (%)</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Average runtime per task (s)</bold>
                </td>
              </tr>
            </thead>
            <tbody>
              <tr>
                <td rowspan="2">Ternary</td>
                <td>Thermo-Calc</td>
                <td>20,000</td>
                <td>20,000</td>
                <td>100.00</td>
                <td>0.011268</td>
              </tr>
              <tr>
                <td>Phase Lab</td>
                <td>20,000</td>
                <td>20,000</td>
                <td>100.00</td>
                <td>0.006933</td>
              </tr>
              <tr>
                <td>9-component</td>
                <td>Phase Lab</td>
                <td>10,000</td>
                <td>9,932</td>
                <td>99.32</td>
                <td>1.122</td>
              </tr>
              <tr>
                <td>12-component</td>
                <td>Phase Lab</td>
                <td>10,000</td>
                <td>9,814</td>
                <td>98.14</td>
                <td>2.19</td>
              </tr>
            </tbody>
          </table>
          <table-wrap-foot>
            <fn>
              <p>Note: Completion rate is defined as the ratio of tasks yielding valid outputs to the total number of submitted tasks.</p>
            </fn>
          </table-wrap-foot>
        </table-wrap>
      </sec>
      <sec id="sec3-2">
        <title>Multicomponent phase equilibria</title>
        <p>Thermodynamic accuracy was assessed by comparing calculated multicomponent phase diagrams with experimental data from the literature. <xref ref-type="fig" rid="fig2">Figure 2A</xref> and <xref ref-type="fig" rid="fig2">B</xref> present the calculated isothermal sections of the Al-Co-Cr and Al-Co-Ni ternary systems at 1,273 K, respectively. The predicted phase boundaries agree well with experimental measurements<sup>[<xref ref-type="bibr" rid="B46">46</xref>,<xref ref-type="bibr" rid="B47">47</xref>]</sup>, reproducing the topology of multiphase regions and the stability ranges of ordered intermetallic phases. To evaluate performance in higher-order systems, <xref ref-type="fig" rid="fig2">Figure 2C</xref> presents the calculated isothermal section at the Al-rich corner of the Al-Cu-Mg-Zn quaternary system. Despite increased compositional complexity, the predicted phase regions remain consistent with experimentally determined boundaries<sup>[<xref ref-type="bibr" rid="B48">48</xref>]</sup>, indicating good performance of the thermodynamic descriptions and equilibrium solver. In addition, <xref ref-type="fig" rid="fig2">Figure 2D</xref> shows a calculated vertical section of the Fe-C-Cr-Mn quaternary system, which is relevant to steel heat-treatment design. The predicted transformation temperatures and phase stability ranges closely match experimental observations<sup>[<xref ref-type="bibr" rid="B49">49</xref>]</sup>, indicating that the equilibrium solver can handle multidimensional composition spaces in the tested cases. Beyond validating thermodynamic accuracy, these multicomponent equilibrium maps - including phase boundaries, transition temperatures, and phase fraction evolution - can be directly exported as structured datasets, providing consistent thermodynamic constraints for AI-assisted surrogate modeling, composition screening, and ICME phase-stability analysis across alloy systems.</p>
        <fig id="fig2" position="float" pdfpage="11">
          <label>Figure 2</label>
          <caption>
            <p>Calculated multicomponent phase diagrams compared with experimental data: (A) isothermal section of the Al-Co-Cr ternary system at 1,273 K<sup>[<xref ref-type="bibr" rid="B46">46</xref>]</sup>; (B) isothermal section of the Al-Co-Ni ternary system at 1,273 K<sup>[<xref ref-type="bibr" rid="B47">47</xref>]</sup>; (C) isothermal section of the Al-Cu-Mg-Zn quaternary system at the Al-rich corner<sup>[<xref ref-type="bibr" rid="B48">48</xref>]</sup>; (D) vertical section of the Fe-C-Cr-Mn quaternary system<sup>[<xref ref-type="bibr" rid="B49">49</xref>]</sup>.</p>
          </caption>
          <graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="jmi6005.fig.2.jpg" />
        </fig>
      </sec>
      <sec id="sec3-3">
        <title>Diffusion and phase transformations</title>
        <p>Diffusion is the fundamental kinetic mechanism governing microstructural evolution and homogenization in multicomponent alloys<sup>[<xref ref-type="bibr" rid="B27">27</xref>]</sup>. Phase Lab validates its kinetic module through a hierarchical approach, starting from atomic mobility and extending to complex precipitation and phase transformation phenomena. This module is benchmarked using diffusion coefficient benchmarks and composition-profile predictions from diffusion-couple simulations. <xref ref-type="fig" rid="fig3">Figure 3A</xref> compares the calculated interdiffusion coefficients for the face-centered cubic (FCC) phase in the binary Ni-Ti system with experimental measurements<sup>[<xref ref-type="bibr" rid="B50">50</xref>]</sup>, showing good agreement. Moving to complex systems, <xref ref-type="fig" rid="fig3">Figure 3B</xref> demonstrates the platform’s capability to simulate composition profiles in the multicomponent Ni-Al-Co-Cr-Ta-Ti-W superalloy. The predicted diffusion paths align closely with high-throughput measurements<sup>[<xref ref-type="bibr" rid="B51">51</xref>]</sup>, supporting the applicability of the mobility database for high-order systems.</p>
        <fig id="fig3" position="float" pdfpage="12">
          <label>Figure 3</label>
          <caption>
            <p>Validation of kinetic simulations regarding diffusion and phase transformations: (A) interdiffusion coefficients for the FCC phase in the binary Ni-Ti<sup>[<xref ref-type="bibr" rid="B50">50</xref>]</sup>; (B) composition profiles in the multicomponent Ni-Al-Co-Cr-Ta-Ti-W superalloy<sup>[<xref ref-type="bibr" rid="B51">51</xref>]</sup>; (C) temporal evolution of number density and (D) mean radius of γ′ precipitates in Ni-5.2Al-14.2Cr (at.%) alloy aged at 600 °C<sup>[<xref ref-type="bibr" rid="B41">41</xref>]</sup>; (E) TTT diagrams for 5140 steel (Fe-0.42C-0.68Mn-0.16Si-0.93Cr, wt.%)<sup>[<xref ref-type="bibr" rid="B53">53</xref>]</sup>; (F) TTT diagram for En36 carburized steel (Fe-0.7C-0.35Mn-0.16Si-3.24Ni-0.96Cr-0.06Mo, wt.%)<sup>[<xref ref-type="bibr" rid="B54">54</xref>]</sup>. FCC: Face-centered cubic; TTT: time-temperature-transformation.</p>
          </caption>
          <graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="jmi6005.fig.3.jpg" />
        </fig>
        <p>Building upon accurate diffusion data, Phase Lab simulates diffusion-controlled phase transformations by combining CALPHAD driving forces with kinetic models (nucleation, growth, and coarsening). <xref ref-type="fig" rid="fig3">Figure 3C</xref> and <xref ref-type="fig" rid="fig3">D</xref> present the calculated temporal evolution of number density and mean radius for γ′ precipitation in a Ni-5.2Al-14.2Cr (at.%) alloy aged at 600 °C. These results show reasonable agreement with measurements<sup>[<xref ref-type="bibr" rid="B41">41</xref>]</sup>, demonstrating that the implemented framework effectively captures the multi-stage precipitation kinetics in multicomponent alloys.</p>
        <p>For steel heat treatment design, TTT and CCT diagrams are critical yet labor-intensive to determine experimentally<sup>[<xref ref-type="bibr" rid="B52">52</xref>]</sup>. Phase Lab enables efficient computation of these diagrams. <xref ref-type="fig" rid="fig3">Figure 3E</xref> and <xref ref-type="fig" rid="fig3">F</xref> compare the calculated TTT diagrams with experimental data for 5140 steel (Fe-0.42C-0.68Mn-0.16Si-0.93Cr, wt.%)<sup>[<xref ref-type="bibr" rid="B53">53</xref>]</sup> and En36 carburized steel (Fe-0.7C-0.35Mn-0.16Si-3.24Ni-0.96Cr-0.06Mo, wt.%)<sup>[<xref ref-type="bibr" rid="B54">54</xref>]</sup>. The agreement in transformation-start and transformation-finish boundaries supports the applicability of the implemented kinetic models to the tested ferrous alloys. The resulting diffusion coefficients, composition profiles, precipitation descriptors, and TTT/CCT boundary points constitute machine-readable kinetic datasets that are directly reusable in ICME process-microstructure models and AI-driven analysis of transformation kinetics.</p>
      </sec>
      <sec id="sec3-4">
        <title>Thermophysical properties</title>
        <p>Accurate prediction of thermophysical properties is essential for process modeling because they govern phenomena such as thermal expansion and melt flow during solidification - as well as for assessing the functional performance of alloys<sup>[<xref ref-type="bibr" rid="B14">14</xref>,<xref ref-type="bibr" rid="B55">55</xref>]</sup>. To address these needs, Phase Lab employs CALPHAD-consistent formulations to evaluate molar volume, viscosity, and transport properties as functions of temperature and composition. Regarding volumetric and rheological behaviors, <xref ref-type="fig" rid="fig4">Figure 4A</xref> compares the calculated linear thermal expansion coefficient of pure FCC Ni against Ref.<sup>[<xref ref-type="bibr" rid="B32">32</xref>]</sup>, showing that the main temperature dependence is reproduced. <xref ref-type="fig" rid="fig4">Figure 4B</xref> compares calculated liquid densities in the Ni-Co-Al ternary system with experiments<sup>[<xref ref-type="bibr" rid="B56">56</xref>]</sup>, showing quantitative agreement across the measured temperature range. For melt rheology, <xref ref-type="fig" rid="fig4">Figure 4C</xref> and <xref ref-type="fig" rid="fig4">D</xref> present calculated liquid viscosities for the Ni-Ta binary and Al-Nb-Ti ternary systems, respectively, again exhibiting good agreement with experimental data<sup>[<xref ref-type="bibr" rid="B57">57</xref>,<xref ref-type="bibr" rid="B58">58</xref>]</sup>. In terms of transport phenomena, <xref ref-type="fig" rid="fig4">Figure 4E</xref> and <xref ref-type="fig" rid="fig4">F</xref> show the calculated thermal conductivities for the hexagonal close-packed (HCP) phase in the Al-Mg binary system and the FCC phase in the Al-Mg-Zn ternary system, respectively. The results show quantitative agreement with experimental data within the tested composition and temperature ranges<sup>[<xref ref-type="bibr" rid="B36">36</xref>,<xref ref-type="bibr" rid="B37">37</xref>]</sup>. For electrical transport, <xref ref-type="fig" rid="fig4">Figure 4G</xref> and <xref ref-type="fig" rid="fig4">H</xref> present electrical conductivity predictions for the FCC phase in the Cu-Mn binary and Cu-Mn-Sn ternary systems, showing good agreement with reported measurements<sup>[<xref ref-type="bibr" rid="B38">38</xref>,<xref ref-type="bibr" rid="B59">59</xref>]</sup>. Collectively, these benchmarks indicate reasonable performance of the implemented physical models, suggesting that Phase Lab can support integrated process simulations, alloy screening, and property optimization. Because these thermophysical properties are evaluated as continuous functions of temperature and composition using CALPHAD-consistent formulations, the resulting property curves and tables can be systematically aggregated into reusable datasets for ICME process simulation and MGE-oriented property mapping.</p>
        <fig id="fig4" position="float" pdfpage="13">
          <label>Figure 4</label>
          <caption>
            <p>Validation of thermophysical properties: (A) linear thermal expansion coefficient of pure FCC Ni<sup>[<xref ref-type="bibr" rid="B32">32</xref>]</sup>; (B) liquid-phase densities in the ternary Ni-Co-Al<sup>[<xref ref-type="bibr" rid="B56">56</xref>]</sup>; (C) viscosity of the binary Ni-Ta<sup>[<xref ref-type="bibr" rid="B57">57</xref>]</sup>; (D) viscosity of the ternary Al-Nb-Ti<sup>[<xref ref-type="bibr" rid="B58">58</xref>]</sup>; (E) thermal conductivity of HCP phase in the binary Al-Mg<sup>[<xref ref-type="bibr" rid="B36">36</xref>]</sup>; (F) thermal conductivity of FCC phase in the ternary Al-Mg-Zn<sup>[<xref ref-type="bibr" rid="B37">37</xref>]</sup>; (G) electrical conductivity of FCC phase in the binary Cu-Mn<sup>[<xref ref-type="bibr" rid="B59">59</xref>]</sup>; (H) electrical conductivity of FCC phase in the ternary Cu-Mn-Sn<sup>[<xref ref-type="bibr" rid="B38">38</xref>]</sup>. FCC: Face-centered cubic; HCP: hexagonal close-packed.</p>
          </caption>
          <graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="jmi6005.fig.4.jpg" />
        </fig>
      </sec>
      <sec id="sec3-5">
        <title>Solidification performance and hot cracking susceptibility</title>
        <p>Solidification behavior critically affects manufacturability and defect formation in casting and additive manufacturing<sup>[<xref ref-type="bibr" rid="B9">9</xref>,<xref ref-type="bibr" rid="B60">60</xref>]</sup>. <xref ref-type="fig" rid="fig5">Figure 5</xref> evaluates the solidification module by comparing calculated solidification paths with experimental data. For the steel case [<xref ref-type="fig" rid="fig5">Figure 5A</xref>], the partial equilibrium approximation is used to account for the fast diffusion of interstitial carbon, showing good agreement with measurements reported by Koshikawa <italic>et al.</italic><sup>[<xref ref-type="bibr" rid="B61">61</xref>]</sup>. For the Ni-based superalloy case [<xref ref-type="fig" rid="fig5">Figure 5B</xref>], the Scheil-Gulliver model captures the segregation behavior of substitutional alloying elements and is consistent with experimental data from Zheng <italic>et al.</italic><sup>[<xref ref-type="bibr" rid="B62">62</xref>]</sup>. These case studies illustrate that Phase Lab flexibly selects appropriate approximations to treat different diffusion regimes and alloy classes.</p>
        <fig id="fig5" position="float" pdfpage="14">
          <label>Figure 5</label>
          <caption>
            <p>Comparison of calculated non-equilibrium solidification paths with experimental data: (A) steel alloy<sup>[<xref ref-type="bibr" rid="B61">61</xref>]</sup>; (B) Ni-based superalloy<sup>[<xref ref-type="bibr" rid="B62">62</xref>]</sup>.</p>
          </caption>
          <graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="jmi6005.fig.5.jpg" />
        </fig>
        <p>For Ni-based superalloys, solidification behavior is closely related to weldability and hot cracking susceptibility because thermal stress and wide freezing ranges often promote crack formation during welding and additive manufacturing<sup>[<xref ref-type="bibr" rid="B2">2</xref>,<xref ref-type="bibr" rid="B12">12</xref>,<xref ref-type="bibr" rid="B60">60</xref>,<xref ref-type="bibr" rid="B63">63</xref>]</sup>. In this context, Phase Lab has also been applied in a recent study on the GH3539 superalloy to analyze the effects of minor alloying additions on solidification-assisted cracking<sup>[<xref ref-type="bibr" rid="B64">64</xref>]</sup>. The calculations showed that Zr significantly widens the solidification temperature range (STR), consistent with its crack-promoting role, whereas C and Si also modify the STR and solidification response but with more complex effects associated with both increased cracking tendency and eutectic-assisted crack filling. These application studies demonstrate that the solidification module can support not only standard path prediction, but also composition-sensitive interpretation of weldability and crack formation in engineering alloys. For broader solidification-related hot-cracking assessment, Phase Lab integrates multiple commonly used cracking indices (<italic>SI</italic>, <italic>CSC</italic>, <italic>CTI</italic>, and <italic>SCI</italic>) within a single workflow. With a consistent non-equilibrium solidification setting, users can obtain all indices and comparative rankings in a single run, with results directly exportable for alloy down-selection. This integrated implementation avoids duplicated and potentially inconsistent recalculation of terminal solidification characteristics (e.g., freezing range and end-of-solidification metrics) and segregation paths across disparate tools, thereby improving computational efficiency and reproducibility for screening purposes. As summarized in <xref ref-type="table" rid="t4">Table 4</xref>, susceptibility criteria were calculated for a set of commercial superalloys. The results indicate that <italic>CSC</italic> and <italic>SCI</italic> show stronger correspondence with experimentally reported printability/weldability for the alloy set considered, whereas <italic>SI</italic> and <italic>CTI</italic> provide weaker discrimination. Alloys with high <italic>CSC</italic>/<italic>SCI</italic> values - such as IN738LC, IN939, CM247LC, and Mar-M247 - are widely reported to exhibit poor weldability and elevated cracking risk<sup>[<xref ref-type="bibr" rid="B2">2</xref>,<xref ref-type="bibr" rid="B65">65</xref>-<xref ref-type="bibr" rid="B67">67</xref>]</sup>, while alloys with lower indices - such as IN718 and the ABD-series alloys - exhibit improved processability<sup>[<xref ref-type="bibr" rid="B2">2</xref>,<xref ref-type="bibr" rid="B13">13</xref>,<xref ref-type="bibr" rid="B31">31</xref>,<xref ref-type="bibr" rid="B68">68</xref>-<xref ref-type="bibr" rid="B71">71</xref>]</sup>. The calculations also quantify the role of minor alloying additions: trace Hf and Zr additions (e.g., in CM247LC and IN939) increase cracking susceptibility by expanding the terminal freezing range, consistent with experimental observations. The integrated, single-run evaluation of multiple solidification cracking indices enables the generation of consistent ranking datasets without duplicated or inconsistent recalculation, which is particularly advantageous for high-throughput alloy down-selection in AI-assisted and ICME-based design workflows.</p>
        <table-wrap id="t4">
          <label>Table 4</label>
          <caption>
            <p>Calculated hot cracking susceptibility criteria (<italic>SI</italic>, <italic>CSC</italic>, <italic>CTI</italic>, and <italic>SCI</italic>) for typical Ni-based superalloys compared with literature data included for comparison</p>
          </caption>
          <table frame="hsides" rules="groups" pdfpage="15">
            <thead>
              <tr>
                <td style="border-bottom:1;" />
                <td style="border-bottom:1;">
                  <bold>Ni</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Al</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>B</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>C</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Co</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Cr</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Fe</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Hf</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Mo</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Nb</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Ta</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Ti</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>W</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>Zr</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>
                    <italic>SI</italic>
                  </bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>
                    <italic>CSC</italic>
                  </bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>
                    <italic>CTI</italic>
                  </bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>
                    <italic>SCI</italic> (<italic>fs</italic> = 0.90-0.99)</bold>
                </td>
                <td style="border-bottom:1;">
                  <bold>
                    <italic>SCI</italic> (<italic>fs</italic> = 0.99)</bold>
                </td>
              </tr>
            </thead>
            <tbody>
              <tr>
                <td>
                  <bold>Mar-M247</bold>
                </td>
                <td>Bal</td>
                <td>5.5</td>
                <td>0.015</td>
                <td>0.15</td>
                <td>10</td>
                <td>8.4</td>
                <td>-</td>
                <td>1.5</td>
                <td>0.7</td>
                <td>-</td>
                <td>3.0</td>
                <td>1.0</td>
                <td>10</td>
                <td>0.05</td>
                <td>128<break />245<sup>[<xref ref-type="bibr" rid="B31">31</xref>]</sup></td>
                <td>2.92</td>
                <td>40<break />40<sup>[<xref ref-type="bibr" rid="B31">31</xref>]</sup></td>
                <td>4,572</td>
                <td>21,626</td>
              </tr>
              <tr>
                <td>
                  <bold>CM247LC</bold>
                </td>
                <td>Bal</td>
                <td>5.6</td>
                <td>0.01</td>
                <td>0.07</td>
                <td>9</td>
                <td>8</td>
                <td>-</td>
                <td>1.4</td>
                <td>0.5</td>
                <td>-</td>
                <td>3.2</td>
                <td>0.7</td>
                <td>10</td>
                <td>0.01</td>
                <td>128<break />238<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>3.2</td>
                <td>40</td>
                <td>5,161<break />15,980<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>28,890</td>
              </tr>
              <tr>
                <td>
                  <bold>CM247LC Hf free</bold>
                </td>
                <td>Bal</td>
                <td>5.6</td>
                <td>0.01</td>
                <td>0.07</td>
                <td>9</td>
                <td>8</td>
                <td>-</td>
                <td>-</td>
                <td>0.5</td>
                <td>-</td>
                <td>3.2</td>
                <td>0.7</td>
                <td>10</td>
                <td>0.01</td>
                <td>81<break />151<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>1.85</td>
                <td>40</td>
                <td>2,001<break />5,036<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>7,733</td>
              </tr>
              <tr>
                <td>
                  <bold>IN939</bold>
                </td>
                <td>Bal</td>
                <td>1.76</td>
                <td>0.009</td>
                <td>0.16</td>
                <td>18.8</td>
                <td>22.1</td>
                <td>-</td>
                <td>0.01</td>
                <td>-</td>
                <td>0.97</td>
                <td>1.37</td>
                <td>3.8</td>
                <td>1.96</td>
                <td>0.11</td>
                <td>172<break />193<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>1.85</td>
                <td>30</td>
                <td>4,194<break />7,170<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>21,291</td>
              </tr>
              <tr>
                <td>
                  <bold>IN939 Zr free</bold>
                </td>
                <td>Bal</td>
                <td>1.76</td>
                <td>0.009</td>
                <td>0.16</td>
                <td>18.8</td>
                <td>22.1</td>
                <td>-</td>
                <td>0.01</td>
                <td>-</td>
                <td>0.97</td>
                <td>1.37</td>
                <td>3.8</td>
                <td>1.96</td>
                <td>-</td>
                <td>155<break />178<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>1.29</td>
                <td>30</td>
                <td>2,692<break />4,352<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>7,111</td>
              </tr>
              <tr>
                <td>
                  <bold>IN718</bold>
                </td>
                <td>Bal</td>
                <td>0.6</td>
                <td>0.005</td>
                <td>0.05</td>
                <td>-</td>
                <td>19</td>
                <td>19</td>
                <td>-</td>
                <td>3</td>
                <td>5</td>
                <td>-</td>
                <td>0.9</td>
                <td>-</td>
                <td>-</td>
                <td>242<break />243<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>0.24</td>
                <td>20</td>
                <td>865<break />921<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>2,696</td>
              </tr>
              <tr>
                <td>
                  <bold>IN738LC</bold>
                </td>
                <td>Bal</td>
                <td>3.4</td>
                <td>0.01</td>
                <td>0.09</td>
                <td>8.5</td>
                <td>16</td>
                <td>-</td>
                <td>-</td>
                <td>1.7</td>
                <td>0.8</td>
                <td>1.7</td>
                <td>3.4</td>
                <td>2.6</td>
                <td>0.06</td>
                <td>135<break />148<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>2.52</td>
                <td>30</td>
                <td>3,537<break />6,681<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>20,628</td>
              </tr>
              <tr>
                <td>
                  <bold>ABD-850AM</bold>
                </td>
                <td>Bal</td>
                <td>1.29</td>
                <td>0.003</td>
                <td>0.01</td>
                <td>8.99</td>
                <td>8.3</td>
                <td>-</td>
                <td>-</td>
                <td>1.89</td>
                <td>0.6</td>
                <td>0.44</td>
                <td>2.22</td>
                <td>4.74</td>
                <td>-</td>
                <td>86<break />142<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>2</td>
                <td>10</td>
                <td>2,318<break />5,545<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>11,711</td>
              </tr>
              <tr>
                <td>
                  <bold>ABD900-AM</bold>
                </td>
                <td>Bal</td>
                <td>2.11</td>
                <td>0.005</td>
                <td>0.05</td>
                <td>19.93</td>
                <td>16.96</td>
                <td>-</td>
                <td>-</td>
                <td>2.09</td>
                <td>1.78</td>
                <td>1.42</td>
                <td>2.39</td>
                <td>3.08</td>
                <td>-</td>
                <td>187<break />198<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>1.16</td>
                <td>42</td>
                <td>2,821<break />3,577<sup>[<xref ref-type="bibr" rid="B2">2</xref>]</sup></td>
                <td>1,063</td>
              </tr>
            </tbody>
          </table>
          <table-wrap-foot>
            <fn>
              <p>Note: Alloy compositions are given in wt.%. “Bal” denotes balance. “-” indicates that the element was not intentionally added or that the corresponding value was not reported, as applicable. <italic>SCI</italic> was evaluated over the solid fraction interval <italic>fs</italic> = 0.90-0.99 and at <italic>fs</italic> = 0.99, as listed in the last two columns; <italic>fs</italic> denotes solid fraction. Higher <italic>CSC</italic> and <italic>SCI</italic> values generally indicate greater hot cracking susceptibility and poorer printability during additive manufacturing. SI: Solidification interval; CSC: Clyne-Davies cracking susceptibility coefficient; CTI: critical temperature interval; SCI: Kou’s solidification cracking index.</p>
            </fn>
          </table-wrap-foot>
        </table-wrap>
      </sec>
      <sec id="sec3-6">
        <title>Mechanical properties</title>
        <p>To evaluate the predictive capability for mechanical performance, Phase Lab was benchmarked against experimental strength and creep data for a wide range of Ni-based superalloys. The strength module combines CALPHAD-derived state variables with physics-based strengthening contributions from solid solution, grain boundaries (Hall-Petch), and precipitation hardening. Experimental datasets for UNS-series alloys were compiled from standard industry references, including Special Metals technical datasheets and ASM handbooks<sup>[<xref ref-type="bibr" rid="B72">72</xref>,<xref ref-type="bibr" rid="B73">73</xref>]</sup>. <xref ref-type="fig" rid="fig6">Figure 6A</xref> and <xref ref-type="fig" rid="fig6">B</xref> compare the calculated room-temperature YS and UTS with experimental values, showing strong linear correlation. To assess thermal responses, <xref ref-type="fig" rid="fig6">Figure 6C</xref> illustrates the temperature-dependent strength evolution of Nimonic 901, where the model reproduces the main experimental trends over the measured range. Extending this validation, <xref ref-type="fig" rid="fig6">Figure 6D</xref> compares calculated and experimental high-temperature YSs across multiple commercial alloys, demonstrating good agreement.</p>
        <fig id="fig6" position="float" pdfpage="17">
          <label>Figure 6</label>
          <caption>
            <p>Validation of strength and creep performance predictions for Ni-based superalloys with experimental data<sup>[<xref ref-type="bibr" rid="B72">72</xref>,<xref ref-type="bibr" rid="B73">73</xref>]</sup>: (A) YS and (B) UTS at room temperature; (C) temperature-dependent strength evolution curve for Nimonic 901; (D) high-temperature YS for various commercial alloys; (E) log(stress) <italic>vs.</italic> log(rupture life) plots for Nimonic 105 at varying temperatures; (F) 1,000-hour rupture strength for various alloys. YS: Yield strength; UTS: ultimate tensile strength.</p>
          </caption>
          <graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="jmi6005.fig.6.jpg" />
        </fig>
        <p>Beyond static strength, Phase Lab integrates thermodynamic and kinetic data to support creep assessment. <xref ref-type="fig" rid="fig6">Figure 6E</xref> presents the calculated log(stress)-log(rupture life) relationships for Nimonic 105 at various temperatures, capturing the general time-dependent trend. <xref ref-type="fig" rid="fig6">Figure 6F</xref> validates the 1,000-hour rupture strength for a broad range of commercial Ni-based alloys. Quantitative error statistics for these datasets are summarized in <xref ref-type="table" rid="t5">Table 5</xref>, where <italic>N</italic> is the number of data points, <italic>R</italic><sup>2</sup> is the coefficient of determination, MAE is the mean absolute error, MAPE is the mean absolute percentage error, and MaxAE is the maximum absolute error. Overall, the strength predictions show reasonable agreement with experiments. The 1,000-hour creep rupture strength predictions capture the general trend across alloys but exhibit larger scatter, and should therefore be regarded as screening-level estimates rather than high-precision lifetime predictions.</p>
        <table-wrap id="t5">
          <label>Table 5</label>
          <caption>
            <p>Summary of prediction errors for mechanical properties (Ni-based superalloys)</p>
          </caption>
          <table frame="hsides" rules="groups" pdfpage="18">
            <thead>
              <tr>
                <td>
                  <bold>Property</bold>
                </td>
                <td>
                  <bold>
                    <italic>N</italic> (data points)</bold>
                </td>
                <td>
                  <bold>
                    <italic>R</italic>
                    <sup>2</sup> (coefficient of determination)</bold>
                </td>
                <td>
                  <bold>MAE (mean absolute error)</bold>
                </td>
                <td>
                  <bold>MAPE (mean absolute percentage error)</bold>
                </td>
                <td>
                  <bold>MaxAE (maximum absolute error)</bold>
                </td>
              </tr>
            </thead>
            <tbody>
              <tr>
                <td>Room-temperature YS</td>
                <td>27</td>
                <td>0.858</td>
                <td>78.8 MPa</td>
                <td>14.2%</td>
                <td>256.8 MPa</td>
              </tr>
              <tr>
                <td>Room-temperature UTS</td>
                <td>28</td>
                <td>0.824</td>
                <td>81.5 MPa</td>
                <td>8.9%</td>
                <td>258.1 MPa</td>
              </tr>
              <tr>
                <td>High-temperature YS</td>
                <td>77</td>
                <td>0.968</td>
                <td>47.5 MPa</td>
                <td>15.9%</td>
                <td>138.4 MPa</td>
              </tr>
              <tr>
                <td>1,000-hour creep rupture strength</td>
                <td>76</td>
                <td>0.878</td>
                <td>41.3 MPa</td>
                <td>26.8%</td>
                <td>317.2 MPa</td>
              </tr>
            </tbody>
          </table>
          <table-wrap-foot>
            <fn>
              <p>YS: Yield strength; UTS: ultimate tensile strength.</p>
            </fn>
          </table-wrap-foot>
        </table-wrap>
        <p>Taken together, the cross-domain comparisons indicate that the integrated CALPHAD-based models provide reasonable agreement with reference data in the tested cases and highlight the value of a consistent CALPHAD-to-data workflow. By exporting results as standardized, provenance-rich data products, Phase Lab enables reproducible aggregation across alloy systems and provides directly reusable inputs for surrogate modeling, screening, and data-driven ICME/MGE workflows that are difficult to realize with ad hoc, tool-specific practices.</p>
      </sec>
    </sec>
    <sec id="sec4">
      <title>CONCLUSIONS</title>
      <p>This work presents Phase Lab as a cloud-native CALPHAD-to-data platform for alloy designers, CALPHAD practitioners, and AI/ICME/MGE researchers who require scalable computation together with standardized data products. The main contribution of the platform is not the development of new thermodynamic or kinetic models, but the standardization of CALPHAD calculations into reproducible, metadata-linked, and machine-readable data products. By integrating server-side computation, task orchestration, provenance tracking, database/model versioning, and structured export, Phase Lab provides a practical route for connecting physics-based calculations with AI/ML, ICME, and MGE workflows.</p>
      <p>The benchmark and validation results demonstrate that Phase Lab can reproduce representative CALPHAD calculations and maintain stable execution in high-throughput settings. In point-to-point ternary benchmarks, Phase Lab matched Thermo-Calc results for molar Gibbs energy, liquidus temperature, and solidus temperature under aligned calculation settings. In batch tests, Phase Lab achieved a 100% completion rate for 20,000 ternary calculations with an average runtime of 0.006933 s per task. For 9-component and 12-component calculations, Phase Lab achieved completion rates of 99.32% and 98.14%, respectively, with average runtimes of 1.122 and 2.19 s per task. Across the validation cases, the platform showed agreement with literature or experimental data for phase equilibria, diffusion and precipitation kinetics, transformation diagrams, thermophysical properties, solidification behavior, hot-cracking indicators, and mechanical properties. For Ni-based superalloys, the room-temperature yield-strength and ultimate-tensile-strength predictions gave <italic>R</italic><sup>2</sup> values of 0.858 and 0.824, respectively.</p>
      <p>The present platform is most reliable within the alloy systems, databases, and model assumptions covered by the implemented thermodynamic, kinetic, mobility, and property descriptions. Its current validation is mainly focused on metallic systems, and extensions to non-metallic materials require suitable databases and further assessment. Some property predictions, especially creep rupture strength, conductivity, and mechanical properties involving detailed precipitate morphology or dislocation evolution, should currently be regarded as screening-level or model-dependent estimates rather than universal high-precision predictions.</p>
      <p>Future work will focus on expanding database coverage, improving user-defined database support, adding uncertainty information to exported data products, and strengthening extensibility for customized property models. Further integration with DFT, MD, phase-field, and finite-element workflows would also allow Phase Lab to serve as a data-oriented bridge between CALPHAD calculations and broader multiscale alloy design.</p>
    </sec>
  </body>
  <back>
    <sec>
      <title>DECLARATIONS</title>
      <sec>
        <title>Acknowledgments</title>
        <p>The authors thank Prof. Xiaogang Lu, Prof. Yong Du, Prof. Libin Liu, Prof. Jianyun Shen, Prof. Weisen Zheng, Prof. Weiwei Xu, Prof. Xiangxi Ye and Prof. Xiaoyu Chong for helpful discussions and support regarding algorithm optimization, thermodynamic database assessment and refinement, and model development.</p>
      </sec>
      <sec>
        <title>Authors’ contributions</title>
        <p>Conceived and designed the study; provided supervision and project administration; and wrote and revised the manuscript: Yan, L.; Liu, X.; Gong, K.; Wang, Y.</p>
        <p>Developed the methodology and computational framework: Yan, L.; Chen, Y.; Wu, Q.; Dong, R.; Zhang, W.</p>
        <p>Performed software development and code implementation: Chen, Y.; Yan, L.</p>
        <p>Optimized databases and curated thermodynamic and mobility data: Wu, Q.; Dong, R.; Zhang, W.</p>
        <p>Collected, organized, and analyzed the validation datasets: Yan, L.; Dong, R.</p>
        <p>All authors read and approved the final manuscript.</p>
      </sec>
      <sec>
        <title>Availability of data and materials</title>
        <p>A representative export example (results and metadata) is available from the corresponding authors upon request. Phase Lab is accessible at <uri xlink:href="https://cloud.hzwtech.com/phase-lab">https://cloud.hzwtech.com/phase-lab</uri>. Please note that access may require account registration and is subject to licensing and user permissions.</p>
      </sec>
      <sec>
        <title>AI and AI-assisted tools statement</title>
        <p>During the preparation of this manuscript, the AI tool GPT-5.4 and Gemini 3.1 were used solely for language editing. These tools did not influence the study design, data collection, analysis, interpretation, or the scientific content of the work. All authors take full responsibility for the accuracy, integrity, and final content of the manuscript.</p>
      </sec>
      <sec>
        <title>Financial support and sponsorship</title>
        <p>None.</p>
      </sec>
      <sec>
        <title>Conflicts of interest</title>
        <p>Liu, X. is the Executive Editor-in-Chief of the journal <italic>Journal of Materials Informatics</italic>, but was not involved in any steps of editorial processing, notably including reviewer selection, manuscript handling, and decision making. Yan, L.; Wu, Q.; Chen, Y.; Dong, R.; Zhang, W.; Gong, K.; Wang, Y. are affiliated with Hongzhiwei Technology (Shanghai) Co., Ltd.</p>
      </sec>
      <sec>
        <title>Ethical approval and consent to participate</title>
        <p>Not applicable.</p>
      </sec>
      <sec>
        <title>Consent for publication</title>
        <p>Not applicable.</p>
      </sec>
      <sec>
        <title>Copyright</title>
        <p>© The Author(s) 2026.</p>
      </sec>
    </sec>
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