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<article xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:mml="http://www.w3.org/1998/Math/MathML" xml:lang="en" article-type="review-article" dtd-version="1.1">
<front>
<journal-meta>
<journal-id journal-id-type="pmc">CMC</journal-id>
<journal-id journal-id-type="nlm-ta">CMC</journal-id>
<journal-id journal-id-type="publisher-id">CMC</journal-id>
<journal-title-group>
<journal-title>Computers, Materials &#x0026; Continua</journal-title>
</journal-title-group>
<issn pub-type="epub">1546-2226</issn>
<issn pub-type="ppub">1546-2218</issn>
<publisher>
<publisher-name>Tech Science Press</publisher-name>
<publisher-loc>USA</publisher-loc>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">68226</article-id>
<article-id pub-id-type="doi">10.32604/cmc.2025.068226</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Review</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Phase Field Simulation of Fracture Behavior in Shape Memory Alloys and Shape Memory Ceramics: A Review</article-title>
<alt-title alt-title-type="left-running-head">Phase Field Simulation of Fracture Behavior in Shape Memory Alloys and Shape Memory Ceramics: A Review</alt-title>
<alt-title alt-title-type="right-running-head">Phase Field Simulation of Fracture Behavior in Shape Memory Alloys and Shape Memory Ceramics: A Review</alt-title>
</title-group>
<contrib-group>
<contrib id="author-1" contrib-type="author">
<name name-style="western"><surname>Hua</surname><given-names>Junhui</given-names></name><xref ref-type="aff" rid="aff-1">1</xref></contrib>
<contrib id="author-2" contrib-type="author">
<name name-style="western"><surname>Xiong</surname><given-names>Junyuan</given-names></name><xref ref-type="aff" rid="aff-2">2</xref></contrib>
<contrib id="author-3" contrib-type="author" corresp="yes">
<name name-style="western"><surname>Xu</surname><given-names>Bo</given-names></name><xref ref-type="aff" rid="aff-1">1</xref><email>boxu@scu.edu.cn</email></contrib>
<contrib id="author-4" contrib-type="author">
<name name-style="western"><surname>Wang</surname><given-names>Chong</given-names></name><xref ref-type="aff" rid="aff-1">1</xref></contrib>
<contrib id="author-5" contrib-type="author">
<name name-style="western"><surname>Wang</surname><given-names>Qingyuan</given-names></name><xref ref-type="aff" rid="aff-1">1</xref></contrib>
<aff id="aff-1"><label>1</label><institution>Failure Mechanics and Engineering Disaster Prevention Key Laboratory of Sichuan Province, Sichuan University</institution>, <addr-line>Chengdu, 610065</addr-line>, <country>China</country></aff>
<aff id="aff-2"><label>2</label><institution>Sichuan Province Key Laboratory of Advanced Structural Materials Mechanical Behavior and Service Safety, School of Mechanics and Aerospace Engineering, Southwest Jiaotong University</institution>, <addr-line>Chengdu, 610031</addr-line>, <country>China</country></aff>
</contrib-group>
<author-notes>
<corresp id="cor1"><label>&#x002A;</label>Corresponding Author: Bo Xu. Email: <email>boxu@scu.edu.cn</email></corresp>
</author-notes>
<pub-date date-type="collection" publication-format="electronic">
<year>2025</year>
</pub-date>
<pub-date date-type="pub" publication-format="electronic">
<day>29</day><month>08</month><year>2025</year>
</pub-date>
<volume>85</volume>
<issue>1</issue>
<fpage>65</fpage>
<lpage>88</lpage>
<history>
<date date-type="received">
<day>23</day>
<month>5</month>
<year>2025</year>
</date>
<date date-type="accepted">
<day>11</day>
<month>7</month>
<year>2025</year>
</date>
</history>
<permissions>
<copyright-statement>&#x00A9; 2025 The Authors.</copyright-statement>
<copyright-year>2025</copyright-year>
<copyright-holder>Published by Tech Science Press.</copyright-holder>
<license xlink:href="https://creativecommons.org/licenses/by/4.0/">
<license-p>This work is licensed under a <ext-link ext-link-type="uri" xlink:type="simple" xlink:href="https://creativecommons.org/licenses/by/4.0/">Creative Commons Attribution 4.0 International License</ext-link>, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.</license-p>
</license>
</permissions>
<self-uri content-type="pdf" xlink:href="TSP_CMC_68226.pdf"></self-uri>
<abstract>
<p>Shape memory alloys (SMAs) and shape memory ceramics (SMCs) exhibit high recovery ability due to the martensitic transformation, which complicates the fracture mechanism of SMAs and SMCs. The phase field method, as a powerful numerical simulation tool, can efficiently resolve the microstructural evolution, multi-field coupling effects, and fracture behavior of SMAs and SMCs. This review begins by presenting the fundamental theoretical framework of the fracture phase field method as applied to SMAs and SMCs, covering key aspects such as the phase field modeling of martensitic transformation and brittle fracture. Subsequently, it systematically examines the phase field simulations of fracture behaviors in SMAs and SMCs, with particular emphasis on how crystallographic orientation, grain size, and grain boundary properties influence the crack propagation. Additionally, the interplay between martensite transformation and fracture mechanisms is analyzed to provide deeper insights into the material responses under mechanical loading. Finally, the review explores future prospects and emerging trends in phase field simulations of SMA and SMC fracture behavior, along with potential advancements in the fracture phase field method itself, including multi-physics coupling and enhanced computational efficiency for large-scale simulations.</p>
</abstract>
<kwd-group kwd-group-type="author">
<kwd>Phase field</kwd>
<kwd>fracture behavior</kwd>
<kwd>shape memory alloy</kwd>
<kwd>shape memory ceramic</kwd>
</kwd-group>
<funding-group>
<award-group id="awg1">
<funding-source>National Natural Science Foundation of China</funding-source>
<award-id>12202294</award-id>
</award-group>
<award-group id="awg2">
<funding-source>Sichuan Science and Technology Program</funding-source>
<award-id>2024NSFSC1346</award-id>
</award-group>
</funding-group>
</article-meta>
</front>
<body>
<sec id="s1">
<label>1</label>
<title>Introduction</title>
<p>Fracture mechanics, which originated during the intense post-World War II era, has remained vigorous vitality and dynamic development [<xref ref-type="bibr" rid="ref-1">1</xref>]. This field focuses on investigating crack initiation, propagation, and eventual material/structural failure under the combined effects of external stress, temperature, defects, and other factors [<xref ref-type="bibr" rid="ref-2">2</xref>&#x2013;<xref ref-type="bibr" rid="ref-4">4</xref>]. Its fundamental objective is to characterize and predict fracture behavior to enhance structural safety and operational reliability [<xref ref-type="bibr" rid="ref-5">5</xref>].</p>
<p>To address complex fracture challenges, a multi-dimensional analytical framework has been developed. The linear elastic fracture mechanics establishes quantitative models for crack propagation in elastic materials [<xref ref-type="bibr" rid="ref-6">6</xref>,<xref ref-type="bibr" rid="ref-7">7</xref>], while elastic-plastic fracture mechanics accurately characterizes fracture behavior in materials exhibiting plastic deformation [<xref ref-type="bibr" rid="ref-8">8</xref>]. Based on the fatigue fracture analysis methods, the failure mechanisms, crack growth rates, and fatigue life predictions can be revealed through cyclic loading experiments [<xref ref-type="bibr" rid="ref-9">9</xref>]. Through the probabilistic models based on statistical mechanics, the influence of microstructural defect distributions on crack propagation paths can be effectively quantified [<xref ref-type="bibr" rid="ref-10">10</xref>]. Additionally, multi-scale and multi-physics numerical approaches (e.g., the extended finite element method) provide high-precision simulation platforms for engineering fracture prediction [<xref ref-type="bibr" rid="ref-11">11</xref>&#x2013;<xref ref-type="bibr" rid="ref-13">13</xref>]. These methods synergize to complement one another, i.e., the combined application of linear elastic fracture mechanics and elastic-plastic fracture mechanics comprehensively resolves fracture dynamics under high strain rates and complex stress states [<xref ref-type="bibr" rid="ref-14">14</xref>], while integrating fatigue analysis with statistical methods significantly improves reliability assessments of structural failure risks under cyclic loading [<xref ref-type="bibr" rid="ref-15">15</xref>].</p>
<p>Despite the success of traditional fracture mechanics in certain applications, its limitations become evident when addressing the phase interface effects, i.e., it is difficult to accurately describe stress redistribution induced by phase transformation and its impact on fracture behavior. Furthermore, uncertainties in material parameter determination and calibration hinder the accuracy and stability of the models. In this context, the phase field method overcomes the shortcomings of traditional approaches in crack path tracking and tip singularity handling by introducing continuous damage variables (fracture order parameters) [<xref ref-type="bibr" rid="ref-16">16</xref>&#x2013;<xref ref-type="bibr" rid="ref-18">18</xref>]. This method not only efficiently resolves dynamic fracture problems but also demonstrates superior computational accuracy and efficiency in aerospace [<xref ref-type="bibr" rid="ref-19">19</xref>,<xref ref-type="bibr" rid="ref-20">20</xref>], energy [<xref ref-type="bibr" rid="ref-21">21</xref>,<xref ref-type="bibr" rid="ref-22">22</xref>], civil engineering [<xref ref-type="bibr" rid="ref-23">23</xref>,<xref ref-type="bibr" rid="ref-24">24</xref>], and biomedical applications [<xref ref-type="bibr" rid="ref-25">25</xref>]. Compared to conventional methods, the phase field method for fracture offers enhanced adaptability, naturally describing crack nucleation, propagation, and bifurcation without predefined crack paths or supplementary fracture criteria.</p>
<p>Shape memory alloys (SMAs) and shape memory ceramics (SMCs) can experience solid-to-solid phase transformations within specific temperature ranges, accompanied by significant latent heat absorption/release, and stress redistribution. In the phase transformation processes, the crack initiation and propagation can generally occur at phase interfaces [<xref ref-type="bibr" rid="ref-26">26</xref>&#x2013;<xref ref-type="bibr" rid="ref-28">28</xref>]. The participation of martensitic transformation (MT) leads to a more complex fracture mechanism of SMAs and SMCs compared to general brittle and elastoplastic materials, and it is difficult to reflect the microstructure-dependent fracture mechanism through traditional fracture mechanics methods. Owing to abovementioned advantages of phase field method, it holds exceptional promise for the fracture behavior of SMAs and SMCs.</p>
<p>This review summarizes the application of the phase field method for fracture in SMAs and SMCs, with a focus on utilizing this method to predict and analyze crack initiation and propagation under mechanical loading. Firstly, the fundamentals of phase field theory for the fracture of SMAs and SMCs are introduced (<xref ref-type="sec" rid="s2">Section 2</xref>); then, the phase field simulations of the fracture behaviors in SMAs and SMCs are reviewed by addressing the effects of crystallographic orientation, grain size, grain boundary, etc. (<xref ref-type="sec" rid="s3">Sections 3</xref> and <xref ref-type="sec" rid="s4">4</xref>); finally, the prospects and potential trends for phase field simulations of the fracture behavior of SMAs and SMCs, as well as future development direction of the fracture phase field method are discussed (<xref ref-type="sec" rid="s5">Section 5</xref>).</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Fundamentals of Phase Field Theory for the Fracture of SMAs and SMCs</title>
<p>The phase field method for the fracture of SMAs and SMCs is a multi-physics simulation framework constructed by coupling the phase field models of MT and fracture. Its core feature lies in introducing an order parameter to describe the continuous evolution from intact to fractured material states and some other order parameters to describe the MT. The phase field model coupling MT and fracture can effectively describe complex fracture behaviors in the presence of MT.</p>
<p>The application of phase field method to fracture analysis in SMAs and SMCs emerged relatively late. In 2018, Zhao et al. [<xref ref-type="bibr" rid="ref-29">29</xref>] first developed a coupled phase field model to investigate the fracture behavior accompanied by MT in a single-crystal zirconia. By unifying the description of MT and crack propagation through different order parameters, this pioneering work established the theoretical foundation for subsequent researches. In 2020, Zhu and Luo [<xref ref-type="bibr" rid="ref-30">30</xref>] improved the model of Zhao et al. [<xref ref-type="bibr" rid="ref-29">29</xref>], proposing a simplified phase field framework based on the energy minimization principle. This refined model enhanced the computational efficiency by appropriately decoupling the interactions between MT potential functions and fracture energy while preserving physical consistency in MT and fracture processes. The phase field models that describe MT and fracture, as well as their coupling will be briefly introduced in the following sections.</p>
<sec id="s2_1">
<label>2.1</label>
<title>Phase Field Model for Martensitic Transformation (MT)</title>
<p>In phase field modeling of MT, the non-conserved order parameters <inline-formula id="ieqn-1"><mml:math id="mml-ieqn-1"><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn><mml:mo>,</mml:mo><mml:mn>2</mml:mn><mml:mo>,</mml:mo><mml:mo>&#x2026;</mml:mo><mml:mo>,</mml:mo><mml:mi>n</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> are typically introduced to describe the transformation between martensite variants and the parent phase (austenite) [<xref ref-type="bibr" rid="ref-31">31</xref>,<xref ref-type="bibr" rid="ref-32">32</xref>]. Here, <inline-formula id="ieqn-2"><mml:math id="mml-ieqn-2"><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2208;</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mn>0</mml:mn><mml:mo>,</mml:mo><mml:mn>1</mml:mn><mml:mo>]</mml:mo></mml:mrow></mml:math></inline-formula> characterizes the phase state, i.e., <inline-formula id="ieqn-3"><mml:math id="mml-ieqn-3"><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math></inline-formula> indicates complete transformation to the <italic>p</italic>-th variant, while <inline-formula id="ieqn-4"><mml:math id="mml-ieqn-4"><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula> corresponds to the parent phase. Based on the Ginzburg-Landau theory, the total free energy of the system is decomposed into chemical free energy <inline-formula id="ieqn-5"><mml:math id="mml-ieqn-5"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>ch</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> and elastic strain energy <inline-formula id="ieqn-6"><mml:math id="mml-ieqn-6"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> [<xref ref-type="bibr" rid="ref-33">33</xref>]:
<disp-formula id="eqn-1"><label>(1)</label><mml:math id="mml-eqn-1" display="block"><mml:mi>F</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>ch</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></disp-formula></p>
<p>The chemical free energy term <inline-formula id="ieqn-7"><mml:math id="mml-ieqn-7"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>ch</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> includes bulk chemical free energy density <inline-formula id="ieqn-8"><mml:math id="mml-ieqn-8"><mml:mi>f</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mo>&#x2026;</mml:mo><mml:mo>,</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and gradient interfacial energy terms, expressed in integral form as [<xref ref-type="bibr" rid="ref-34">34</xref>,<xref ref-type="bibr" rid="ref-35">35</xref>]:
<disp-formula id="eqn-2"><label>(2)</label><mml:math id="mml-eqn-2" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>ch</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>[</mml:mo><mml:mi>f</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mo>&#x2026;</mml:mo><mml:mo>,</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>p</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:munderover><mml:msub><mml:mi>&#x03B2;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:msub><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mo>&#x22C5;</mml:mo><mml:msub><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula>where <inline-formula id="ieqn-9"><mml:math id="mml-ieqn-9"><mml:msub><mml:mi>&#x03B2;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is the gradient energy coefficient tensor for the <italic>p</italic>-th variant, whose positive definiteness ensures the positive-definite nature of the interfacial energy. For isotropic interfacial energy, <inline-formula id="ieqn-10"><mml:math id="mml-ieqn-10"><mml:msub><mml:mi>&#x03B2;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is simplified to <inline-formula id="ieqn-11"><mml:math id="mml-ieqn-11"><mml:mi>&#x03B2;</mml:mi><mml:msub><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> (<inline-formula id="ieqn-12"><mml:math id="mml-ieqn-12"><mml:msub><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the Kronecker delta).</p>
<p>The elastic strain energy <inline-formula id="ieqn-13"><mml:math id="mml-ieqn-13"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula>, arising from lattice distortion, is expressed using Voigt notation as:
<disp-formula id="eqn-3"><label>(3)</label><mml:math id="mml-eqn-3" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msub><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula>where <inline-formula id="ieqn-14"><mml:math id="mml-ieqn-14"><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the fourth-order elasticity tensor. The elastic strain <inline-formula id="ieqn-15"><mml:math id="mml-ieqn-15"><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula> is defined as the difference between the total strain <inline-formula id="ieqn-16"><mml:math id="mml-ieqn-16"><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>tot</mml:mtext></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula> and the stress-free eigenstrain <inline-formula id="ieqn-17"><mml:math id="mml-ieqn-17"><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msubsup></mml:math></inline-formula>, expressed as:
<disp-formula id="eqn-4"><label>(4)</label><mml:math id="mml-eqn-4" display="block"><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>=</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>tot</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>&#x2212;</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msubsup><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mo>,</mml:mo><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>,</mml:mo><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:munder><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:munder><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mn>00</mml:mn></mml:mrow></mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:msubsup><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup></mml:math></disp-formula>where <inline-formula id="ieqn-18"><mml:math id="mml-ieqn-18"><mml:msub><mml:mi>u</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> denotes the displacement field, and <inline-formula id="ieqn-19"><mml:math id="mml-ieqn-19"><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mn>00</mml:mn></mml:mrow></mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:mi>p</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> represents the stress-free transformation strain associated with the <italic>p</italic>-th martensite variant [<xref ref-type="bibr" rid="ref-33">33</xref>,<xref ref-type="bibr" rid="ref-36">36</xref>].</p>
</sec>
<sec id="s2_2">
<label>2.2</label>
<title>Phase Field Model for Fracture</title>
<p>Based on the fracture phase field theoretical framework developed by Hou et al. [<xref ref-type="bibr" rid="ref-37">37</xref>], a double-well order parameter <inline-formula id="ieqn-20"><mml:math id="mml-ieqn-20"><mml:mi>&#x03D5;</mml:mi><mml:mo>&#x2208;</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn><mml:mo>,</mml:mo><mml:mn>1</mml:mn><mml:mo>]</mml:mo></mml:mrow></mml:math></inline-formula> is introduced to characterize the material damage states, i.e., <inline-formula id="ieqn-21"><mml:math id="mml-ieqn-21"><mml:mi>&#x03D5;</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math></inline-formula> corresponds to the intact phase (crack-free state), while <inline-formula id="ieqn-22"><mml:math id="mml-ieqn-22"><mml:mi>&#x03D5;</mml:mi><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn></mml:math></inline-formula> represents the fully fractured phase (crack region). The total free energy of the system comprises gradient energy, local free energy, and elastic energy [<xref ref-type="bibr" rid="ref-38">38</xref>]:
<disp-formula id="eqn-5"><label>(5)</label><mml:math id="mml-eqn-5" display="block"><mml:mi>E</mml:mi><mml:mo>=</mml:mo><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>gr</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>loc</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula></p>
<p>The gradient energy density <inline-formula id="ieqn-23"><mml:math id="mml-ieqn-23"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>gr</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula>, characterizing the diffuse interfacial energy of the crack surface, is expressed as:
<disp-formula id="eqn-6"><label>(6)</label><mml:math id="mml-eqn-6" display="block"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>gr</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mi>&#x03BE;</mml:mi><mml:mn>2</mml:mn></mml:mfrac><mml:msup><mml:mrow><mml:mo>|</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mi>&#x03D5;</mml:mi><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></disp-formula></p>
<p>The local free energy density <inline-formula id="ieqn-24"><mml:math id="mml-ieqn-24"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>loc</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> is adopted as a double-well potential form:
<disp-formula id="eqn-7"><label>(7)</label><mml:math id="mml-eqn-7" display="block"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>loc</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mi>&#x03BE;</mml:mi><mml:mrow><mml:mn>4</mml:mn><mml:msup><mml:mi>&#x03BA;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:msup><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></disp-formula>where <inline-formula id="ieqn-25"><mml:math id="mml-ieqn-25"><mml:mi>&#x03BE;</mml:mi><mml:mo>&#x003E;</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula> is the mixing energy density, <inline-formula id="ieqn-26"><mml:math id="mml-ieqn-26"><mml:mi>&#x03BA;</mml:mi></mml:math></inline-formula> controls the thickness of the phase field interfacial transition layer, and <inline-formula id="ieqn-27"><mml:math id="mml-ieqn-27"><mml:mi>&#x03BE;</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-28"><mml:math id="mml-ieqn-28"><mml:mi>&#x03BA;</mml:mi></mml:math></inline-formula> satisfy <inline-formula id="ieqn-29"><mml:math id="mml-ieqn-29"><mml:mi>&#x03BE;</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mn>3</mml:mn><mml:mi>&#x03B3;</mml:mi><mml:mi>&#x03BA;</mml:mi></mml:mrow><mml:msqrt><mml:mn>8</mml:mn></mml:msqrt></mml:mfrac></mml:math></inline-formula> (<inline-formula id="ieqn-30"><mml:math id="mml-ieqn-30"><mml:mi>&#x03B3;</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow></mml:msub><mml:mn>2</mml:mn></mml:mfrac></mml:math></inline-formula>, where <inline-formula id="ieqn-31"><mml:math id="mml-ieqn-31"><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the fracture energy) [<xref ref-type="bibr" rid="ref-38">38</xref>,<xref ref-type="bibr" rid="ref-39">39</xref>].</p>
<p>Coupled with the order parameter, the elastic energy density is defined as:
<disp-formula id="eqn-8"><label>(8)</label><mml:math id="mml-eqn-8" display="block"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mi>E</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow><mml:mrow><mml:mn>2</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:mi>&#x03BD;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BD;</mml:mi></mml:mrow></mml:mfrac><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>+</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-32"><mml:math id="mml-ieqn-32"><mml:mi>E</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mi>E</mml:mi><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> represents the elastic modulus of the material, <inline-formula id="ieqn-33"><mml:math id="mml-ieqn-33"><mml:mi>&#x03BD;</mml:mi></mml:math></inline-formula> is Poisson&#x2019;s ratio, <inline-formula id="ieqn-34"><mml:math id="mml-ieqn-34"><mml:mi>E</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-35"><mml:math id="mml-ieqn-35"><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> denote the elastic moduli of the intact and fractured phases, respectively, and <inline-formula id="ieqn-36"><mml:math id="mml-ieqn-36"><mml:mi>h</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mrow><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:mn>4</mml:mn></mml:mrow><mml:msup><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mn>3</mml:mn></mml:mrow></mml:msup><mml:mo>+</mml:mo><mml:mrow><mml:mn>3</mml:mn></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:mn>4</mml:mn></mml:mrow><mml:mi>&#x03D5;</mml:mi><mml:mo>+</mml:mo><mml:mrow><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:math></inline-formula> is the interpolation function.</p>
<p>To eliminate unphysical compressive fracture behavior, Hou et al. [<xref ref-type="bibr" rid="ref-37">37</xref>] incorporate the strain decomposition concept from Amor et al. [<xref ref-type="bibr" rid="ref-40">40</xref>], splitting the elastic energy density into two components:
<disp-formula id="eqn-9"><label>(9)</label><mml:math id="mml-eqn-9" display="block"><mml:msub><mml:mi>f</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:msub><mml:mi>K</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mn>2</mml:mn></mml:mfrac><mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mo>+</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mo>[</mml:mo><mml:mfrac><mml:msub><mml:mi>K</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mn>2</mml:mn></mml:mfrac><mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>+</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mi>&#x03BC;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mi>n</mml:mi></mml:mfrac><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:msub><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mi>n</mml:mi></mml:mfrac><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>l</mml:mi><mml:mi>l</mml:mi></mml:mrow><mml:mrow><mml:mi>e</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msubsup><mml:msub><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>]</mml:mo></mml:mrow></mml:math></disp-formula>where
<disp-formula id="eqn-10"><label>(10)</label><mml:math id="mml-eqn-10" display="block"><mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mrow><mml:mo>&#x27E8;</mml:mo><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x27E9;</mml:mo></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>{</mml:mo><mml:mtable columnalign="left left" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mrow><mml:mtext>if&#xA0;</mml:mtext></mml:mrow><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x003C;</mml:mo><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:mtext>else</mml:mtext></mml:mrow></mml:mtd></mml:mtr></mml:mtable><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo></mml:mrow></mml:math></disp-formula>
<disp-formula id="eqn-11"><label>(11)</label><mml:math id="mml-eqn-11" display="block"><mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>+</mml:mo></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mrow><mml:mo>&#x27E8;</mml:mo><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x27E9;</mml:mo></mml:mrow><mml:mrow><mml:mo>+</mml:mo></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>{</mml:mo><mml:mtable columnalign="left left" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mtd><mml:mtd><mml:mrow><mml:mtext>if&#xA0;</mml:mtext></mml:mrow><mml:mi>t</mml:mi><mml:mi>r</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2265;</mml:mo><mml:mn>0</mml:mn></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mn>0</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:mtext>else</mml:mtext></mml:mrow></mml:mtd></mml:mtr></mml:mtable><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-37"><mml:math id="mml-ieqn-37"><mml:mi>&#x03B4;</mml:mi></mml:math></inline-formula> is a small numerical parameter satisfying <inline-formula id="ieqn-38"><mml:math id="mml-ieqn-38"><mml:msub><mml:mi>E</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mi>E</mml:mi></mml:math></inline-formula>, <inline-formula id="ieqn-39"><mml:math id="mml-ieqn-39"><mml:msub><mml:mi>K</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mi>&#x03BB;</mml:mi><mml:mo>+</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BC;</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mi>n</mml:mi></mml:math></inline-formula> is the bulk modulus (<italic>n</italic> is the spatial dimension), and <inline-formula id="ieqn-40"><mml:math id="mml-ieqn-40"><mml:mi>&#x03BB;</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mn>2</mml:mn><mml:mi>&#x03BC;</mml:mi><mml:mi>&#x03BD;</mml:mi></mml:mrow><mml:mrow><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mn>2</mml:mn><mml:mi>&#x03BD;</mml:mi></mml:mrow></mml:mfrac></mml:math></inline-formula> and <inline-formula id="ieqn-41"><mml:math id="mml-ieqn-41"><mml:mi>&#x03BC;</mml:mi><mml:mo>=</mml:mo><mml:mfrac><mml:mi>E</mml:mi><mml:mrow><mml:mn>2</mml:mn><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:mi>&#x03BD;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:mfrac></mml:math></inline-formula> are the Lam&#x00E9; constants.</p>
</sec>
<sec id="s2_3">
<label>2.3</label>
<title>Phase Field Model Coupling Martensitic Transformation and Fracture</title>
<p>The coupling between MT and crack propagation, as critical microscopic mechanisms of fracture in the materials with MT, has been experimentally and numerically validated. To quantitatively characterize the coupling mechanism between MT and fracture, Zhu and Luo [<xref ref-type="bibr" rid="ref-30">30</xref>] established the coupled phase field model integrating MT and fracture, describing their interactions through a unified free energy functional:
<disp-formula id="eqn-12"><label>(12)</label><mml:math id="mml-eqn-12" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>tot</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>ch</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>gr</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>loc</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></disp-formula></p>
<p>The specific forms of the energy terms are as follows:</p>
<p><bold>Phase transformation chemical free energy</bold> (inherited from <xref ref-type="disp-formula" rid="eqn-2">Eq. (2)</xref>):
<disp-formula id="eqn-13"><label>(13)</label><mml:math id="mml-eqn-13" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>ch</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>[</mml:mo><mml:mi>f</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>,</mml:mo><mml:mo>&#x2026;</mml:mo><mml:mo>,</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:mfrac><mml:mi>&#x03B2;</mml:mi><mml:mn>2</mml:mn></mml:mfrac><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>p</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:munderover><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula></p>
<p><bold>Crack gradient energy</bold> (modified from <xref ref-type="disp-formula" rid="eqn-6">Eq. (6)</xref>):
<disp-formula id="eqn-14"><label>(14)</label><mml:math id="mml-eqn-14" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>gr</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mi>&#x03BE;</mml:mi><mml:mn>2</mml:mn></mml:mfrac><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:msup><mml:mrow><mml:mo>|</mml:mo><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mi>&#x03D5;</mml:mi><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula></p>
<p><bold>Crack local energy</bold> (inherited from <xref ref-type="disp-formula" rid="eqn-7">Eq. (7)</xref>):
<disp-formula id="eqn-15"><label>(15)</label><mml:math id="mml-eqn-15" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>loc</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mfrac><mml:mi>&#x03BE;</mml:mi><mml:mrow><mml:mn>4</mml:mn><mml:msup><mml:mi>&#x03BA;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:msup><mml:mi>&#x03D5;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>)</mml:mo></mml:mrow><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>+</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula></p>
<p><bold>Elastic energy</bold> (improved from <xref ref-type="disp-formula" rid="eqn-9">Eq. (9)</xref>):
<disp-formula id="eqn-16"><label>(16)</label><mml:math id="mml-eqn-16" display="block"><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mi>V</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>[</mml:mo><mml:mfrac><mml:msub><mml:mi>K</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mn>2</mml:mn></mml:mfrac><mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mrow><mml:mo>[</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mo>+</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03B4;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mi>h</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03D5;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:msub><mml:mi>K</mml:mi><mml:mrow><mml:mi>n</mml:mi></mml:mrow></mml:msub><mml:mn>2</mml:mn></mml:mfrac><mml:msubsup><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>+</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:mi>&#x03BC;</mml:mi><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mi>n</mml:mi></mml:mfrac><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:msub><mml:mi>&#x03B4;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>)</mml:mo></mml:mrow><mml:mo>]</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>V</mml:mi></mml:math></disp-formula></p>
<p>The evolution of order parameters are governed via the time-dependent Ginzburg-Landau (TDGL) equations:
<disp-formula id="eqn-17"><label>(17)</label><mml:math id="mml-eqn-17" display="block"><mml:mrow><mml:mo>{</mml:mo><mml:mtable columnalign="left left" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>L</mml:mi><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi>&#x03B4;</mml:mi><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>tot</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi>&#x03B4;</mml:mi><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>p</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mtd></mml:mtr><mml:mtr><mml:mtd><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>&#x03D5;</mml:mi></mml:mrow><mml:mrow><mml:mi mathvariant="normal">&#x2202;</mml:mi><mml:mi>t</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:mi>M</mml:mi><mml:mstyle displaystyle="true" scriptlevel="0"><mml:mfrac><mml:mrow><mml:mi>&#x03B4;</mml:mi><mml:msub><mml:mi>F</mml:mi><mml:mrow><mml:mrow><mml:mtext>tot</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mi>&#x03B4;</mml:mi><mml:mi>&#x03D5;</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mtd></mml:mtr></mml:mtable><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo></mml:mrow></mml:math></disp-formula>where <italic>L</italic> and <italic>M</italic> are the kinetic coefficients.</p>
<p>The mechanical equilibrium condition is written as:
<disp-formula id="eqn-18"><label>(18)</label><mml:math id="mml-eqn-18" display="block"><mml:mi mathvariant="normal">&#x2207;</mml:mi><mml:mo>&#x22C5;</mml:mo><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi><mml:mo>=</mml:mo><mml:mrow><mml:mtext mathvariant="bold">0</mml:mtext></mml:mrow></mml:math></disp-formula></p>
<p>The Cauchy stress tensor <inline-formula id="ieqn-42"><mml:math id="mml-ieqn-42"><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi></mml:math></inline-formula> is derived from Hooke&#x2019;s law as:
<disp-formula id="eqn-19"><label>(19)</label><mml:math id="mml-eqn-19" display="block"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msub><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup></mml:math></disp-formula>where <inline-formula id="ieqn-43"><mml:math id="mml-ieqn-43"><mml:msub><mml:mi>C</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the elasticity modulus tensor, and <inline-formula id="ieqn-44"><mml:math id="mml-ieqn-44"><mml:msubsup><mml:mi>&#x03B5;</mml:mi><mml:mrow><mml:mi>k</mml:mi><mml:mi>l</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>el</mml:mtext></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula> is the elastic strain defined in <xref ref-type="disp-formula" rid="eqn-4">Eq. (4)</xref>.</p>
</sec>
<sec id="s2_4">
<label>2.4</label>
<title>Recent Developments in Fracture Phase Field Models for SMAs and SMCs</title>
<p>Considering the coupling characteristics and energy equation definitions of phase field method, this method can be adapted to construct application-specific phase field models through appropriate modifications. Leveraging this flexibility, researchers have focused on enhancing simulation accuracy by integrating advanced theories and technologies to optimize and innovate the phase field models coupling MT and fracture, thereby advancing the development of phase field method.</p>
<p>The advancement of fracture phase field method has consistently aimed at simulating and predicting crack propagation in complex environments. Schmitt et al. [<xref ref-type="bibr" rid="ref-41">41</xref>] developed a MT-damage coupled phase field model to address tension-compression asymmetry induced by transformation-induced eigenstrain during MT [<xref ref-type="bibr" rid="ref-42">42</xref>]. This model successfully revealed the dynamic interactions between microcrack propagation and martensite formation. A damage variable <inline-formula id="ieqn-45"><mml:math id="mml-ieqn-45"><mml:mi>s</mml:mi></mml:math></inline-formula> (where <inline-formula id="ieqn-46"><mml:math id="mml-ieqn-46"><mml:mi>s</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:math></inline-formula> presents the intact material and <inline-formula id="ieqn-47"><mml:math id="mml-ieqn-47"><mml:mi>s</mml:mi><mml:mo>=</mml:mo><mml:mn>0</mml:mn></mml:math></inline-formula> denotes the fully fractured regions) was employed, governed by the TDGL equation:
<disp-formula id="eqn-20"><label>(20)</label><mml:math id="mml-eqn-20" display="block"><mml:mrow><mml:mover><mml:mi>s</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>M</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mfrac><mml:mrow><mml:mi>&#x03B4;</mml:mi><mml:mi>&#x03C0;</mml:mi></mml:mrow><mml:mrow><mml:mi>&#x03B4;</mml:mi><mml:mi>s</mml:mi></mml:mrow></mml:mfrac><mml:mo>=</mml:mo><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>M</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mo>[</mml:mo><mml:mn>2</mml:mn><mml:mi>s</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03C8;</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03B7;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mfrac><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mn>2</mml:mn><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>s</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>2</mml:mn><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:mi>s</mml:mi><mml:mo>]</mml:mo></mml:mrow></mml:math></disp-formula>where <inline-formula id="ieqn-48"><mml:math id="mml-ieqn-48"><mml:msub><mml:mi>M</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the mobility parameter controlling the damage evolution rate, <inline-formula id="ieqn-49"><mml:math id="mml-ieqn-49"><mml:mi>&#x03C0;</mml:mi></mml:math></inline-formula> is the total energy (including phase field and fracture energies, see Ref. [<xref ref-type="bibr" rid="ref-43">43</xref>]); <inline-formula id="ieqn-50"><mml:math id="mml-ieqn-50"><mml:msub><mml:mi>&#x03C8;</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the phase field potential coupled with <inline-formula id="ieqn-51"><mml:math id="mml-ieqn-51"><mml:mi>s</mml:mi></mml:math></inline-formula>, <inline-formula id="ieqn-52"><mml:math id="mml-ieqn-52"><mml:mi>&#x03B7;</mml:mi></mml:math></inline-formula> is the residual stiffness, <inline-formula id="ieqn-53"><mml:math id="mml-ieqn-53"><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is the crack resistance (equivalent to fracture toughness), and <inline-formula id="ieqn-54"><mml:math id="mml-ieqn-54"><mml:msub><mml:mi>L</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is a characteristic length parameter regulating the crack width. This energy-coupled framework established the foundation for subsequent multi-field modeling.</p>
<p>Kavvadias and Baxevanis [<xref ref-type="bibr" rid="ref-44">44</xref>] developed a thermo-mechanical fracture phase field model for single-crystal NiTi alloys under quasi-static loading (neglecting latent heat), slow thermal loading (assuming uniform temperature distribution), and metastable austenite temperature constraints. Two critical mechanisms were introduced into the model, i.e., a rule-of-mixtures-based coupling of reversible MT and a constitutive law of austenite plasticity formulated via kinematic decomposition of strains [<xref ref-type="bibr" rid="ref-45">45</xref>]. To improve the coupling accuracy, an interaction term was incorporated into the free energy expression derived from Mori-Tanaka and Kr&#x00F6;ner&#x2019;s micromechanical assumptions [<xref ref-type="bibr" rid="ref-46">46</xref>]:<disp-formula id="eqn-21"><label>(21)</label><mml:math id="mml-eqn-21" display="block"><mml:msub><mml:mrow><mml:mover><mml:mi>&#x03C8;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mrow><mml:mtext>int</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mrow><mml:mtext mathvariant="bold">C</mml:mtext></mml:mrow><mml:mo>&#x003A;</mml:mo><mml:msup><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mrow><mml:mrow><mml:mtext>e</mml:mtext></mml:mrow></mml:mrow></mml:msup><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x003A;</mml:mo><mml:msup><mml:mrow><mml:mover><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mrow><mml:mtext>p</mml:mtext></mml:mrow></mml:mrow></mml:msup><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow></mml:msub><mml:mo>&#x003A;</mml:mo><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:mi>&#x03BE;</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:munderover><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>l</mml:mi><mml:mo>=</mml:mo><mml:mn>1</mml:mn></mml:mrow><mml:mrow><mml:msub><mml:mi>N</mml:mi><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:mrow></mml:munderover><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:msubsup><mml:mrow><mml:mover><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mrow><mml:mtext>p</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup><mml:msubsup><mml:mrow><mml:mover><mml:mi>&#x03B3;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup></mml:math></disp-formula>where <inline-formula id="ieqn-55"><mml:math id="mml-ieqn-55"><mml:msup><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mrow><mml:mrow><mml:mtext>e</mml:mtext></mml:mrow></mml:mrow></mml:msup></mml:math></inline-formula> is the elastic strain tensor, <inline-formula id="ieqn-56"><mml:math id="mml-ieqn-56"><mml:msup><mml:mrow><mml:mover><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mrow><mml:mtext>p</mml:mtext></mml:mrow></mml:mrow></mml:msup></mml:math></inline-formula> is the plastic strain rate, <inline-formula id="ieqn-57"><mml:math id="mml-ieqn-57"><mml:msub><mml:mi mathvariant="bold-italic">&#x03C3;</mml:mi><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula> is the average austenite stress, <inline-formula id="ieqn-58"><mml:math id="mml-ieqn-58"><mml:mi>&#x03BE;</mml:mi><mml:mo>=</mml:mo><mml:munder><mml:mo>&#x2211;</mml:mo><mml:mrow><mml:mi>&#x03B1;</mml:mi></mml:mrow></mml:munder><mml:msup><mml:mi>&#x03BE;</mml:mi><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B1;</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msup></mml:math></inline-formula> is the total martensite volume fraction, <inline-formula id="ieqn-59"><mml:math id="mml-ieqn-59"><mml:mmultiscripts><mml:mrow><mml:mover><mml:mi mathvariant="bold-italic">&#x03B5;</mml:mi><mml:mo stretchy="false">&#x005E;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mtext>p</mml:mtext></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mprescripts/><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow><mml:none/></mml:mmultiscripts><mml:mo>=</mml:mo><mml:mfrac><mml:mn>1</mml:mn><mml:mn>2</mml:mn></mml:mfrac><mml:mrow><mml:mo>(</mml:mo><mml:msubsup><mml:mrow><mml:mtext mathvariant="bold">q</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup><mml:mo>&#x2297;</mml:mo><mml:msubsup><mml:mrow><mml:mtext mathvariant="bold">r</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup><mml:mo>+</mml:mo><mml:msubsup><mml:mrow><mml:mtext mathvariant="bold">r</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup><mml:mo>&#x2297;</mml:mo><mml:msubsup><mml:mrow><mml:mtext mathvariant="bold">q</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> is the orientation tensor for the <italic>l</italic>-th slip system, and <inline-formula id="ieqn-60"><mml:math id="mml-ieqn-60"><mml:msubsup><mml:mrow><mml:mtext mathvariant="bold">q</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula>, <inline-formula id="ieqn-61"><mml:math id="mml-ieqn-61"><mml:msubsup><mml:mrow><mml:mtext mathvariant="bold">r</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula>, and <inline-formula id="ieqn-62"><mml:math id="mml-ieqn-62"><mml:msubsup><mml:mrow><mml:mover><mml:mi>&#x03B3;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mrow><mml:mrow><mml:mtext>A</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>l</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula> represent the shear direction, slip plane normal, and average shear rate of the <italic>l</italic>-th slip system. This formulation explicitly quantifies the interplay between MT and plastic deformation through stress-strain coupling. Numerical simulations demonstrated that the model could reasonably capture the transformation-induced toughening, actuation-driven fracture under constant bias loading, and crystallographic orientation dependence of crack morphology, thereby providing critical theoretical support for fracture prediction in the NiTi SMAs under complex mechanical conditions.</p>
<p>The phase field method provides an effective approach for modeling the fatigue crack propagation behavior. Simoes and Mart&#x00ED;nez-Pa&#x00F1;eda [<xref ref-type="bibr" rid="ref-47">47</xref>] developed a phase field framework incorporating elastic strain energy and transformation strain energy, based on an SMA constitutive model that considers both constant fracture energy and the fracture energy dependent on the martensitic volume fraction (via a rule of mixtures). By implementing an efficient implicit time integration scheme, Simoes and Mart&#x00ED;nez-Pa&#x00F1;eda [<xref ref-type="bibr" rid="ref-47">47</xref>] successfully addressed the fatigue fracture problems under complex boundary conditions. Numerical validation demonstrated the model&#x2019;s exceptional capability in simulating multi-crack propagation in SMAs. Hasan et al. [<xref ref-type="bibr" rid="ref-48">48</xref>] proposed two innovative models: In the first one, a fatigue history variable was introduced to modify the fracture toughness parameters, accurately reproducing the characteristics of experimental W&#x00F6;hler curve [<xref ref-type="bibr" rid="ref-49">49</xref>]; in the second one, a finite-strain formulation that coupled reversible MT, martensite reorientation, temperature- and load-dependent hysteresis width, as well as asymmetry between forward and reverse MT was developed, enabling precise predictions of complex MT-fracture interactions.</p>
<p>Recently, the phase field model in fatigue fracture modeling have been further advanced. Simoes et al. [<xref ref-type="bibr" rid="ref-50">50</xref>] established a generalized numerical framework combining phase-field fracture theory, a Drucker-Prager-based constitutive model for SMAs, and fatigue degradation functions. They incorporated AT1 and AT2 phase field methods [<xref ref-type="bibr" rid="ref-51">51</xref>,<xref ref-type="bibr" rid="ref-52">52</xref>], establishing a universal methodology. The bulk energy density and surface energy density were introduced into the governing equations, along with a fatigue degradation function, enabling multi-physics coupling analysis. For the fatigue degradation, the asymptotic analysis of Carrara et al. [<xref ref-type="bibr" rid="ref-53">53</xref>] inspired the adoption of a piecewise function:<disp-formula id="eqn-22"><label>(22)</label><mml:math id="mml-eqn-22" display="block"><mml:mi>f</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:mrow><mml:mo>{</mml:mo><mml:mtable columnalign="center center center" rowspacing="4pt" columnspacing="1em"><mml:mtr><mml:mtd><mml:mn>1</mml:mn></mml:mtd><mml:mtd><mml:mrow><mml:mtext>if</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2264;</mml:mo><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msub></mml:mtd><mml:mtd /></mml:mtr><mml:mtr><mml:mtd><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mn>2</mml:mn><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>+</mml:mo><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:mtd><mml:mtd><mml:mrow><mml:mtext>if</mml:mtext></mml:mrow><mml:mtext>&#x00A0;</mml:mtext><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>&#x2265;</mml:mo><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msub></mml:mtd><mml:mtd /></mml:mtr></mml:mtable><mml:mo fence="true" stretchy="true" symmetric="true"></mml:mo></mml:mrow></mml:math></disp-formula>where the fatigue threshold parameter <inline-formula id="ieqn-63"><mml:math id="mml-ieqn-63"><mml:msub><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mi>T</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> is defined as a time-integrated measure, i.e., <inline-formula id="ieqn-64"><mml:math id="mml-ieqn-64"><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo accent="false">&#x00AF;</mml:mo></mml:mover><mml:mrow><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mo>=</mml:mo><mml:msubsup><mml:mo>&#x222B;</mml:mo><mml:mrow><mml:mn>0</mml:mn></mml:mrow><mml:mrow><mml:mi>t</mml:mi></mml:mrow></mml:msubsup><mml:mi>H</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mi>&#x03B1;</mml:mi><mml:mrow><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mo>|</mml:mo><mml:mrow><mml:mover><mml:mi>&#x03B1;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mo>|</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>t</mml:mi></mml:math></inline-formula>. Coupling this function with SMA constitutive laws yielded a self-evolving fracture phase field model for fatigue crack propagation.</p>
<p>From an energy evolution perspective, Abdollahi and Arias [<xref ref-type="bibr" rid="ref-54">54</xref>] developed a phase field model for the crack propagation in ferroelectric anisotropic polycrystalline BaTiO<sub>3</sub>. A modified fracture surface energy <inline-formula id="ieqn-65"><mml:math id="mml-ieqn-65"><mml:msubsup><mml:mi>G</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>polycrystalline</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>=</mml:mo><mml:msubsup><mml:mi>G</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow><mml:mrow><mml:mrow><mml:mtext>bulk</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mi>F</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> was introduced, where <inline-formula id="ieqn-66"><mml:math id="mml-ieqn-66"><mml:mi>F</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mi>i</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> governs the reduction of critical strain energy release rate along weakened GBs. Emdadi and Zaeem [<xref ref-type="bibr" rid="ref-55">55</xref>] developed a modified Griffith-based phase field framework incorporating two correction parameters (<inline-formula id="ieqn-67"><mml:math id="mml-ieqn-67"><mml:mi>A</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-68"><mml:math id="mml-ieqn-68"><mml:mi>B</mml:mi></mml:math></inline-formula>) to decouple material strength from the regularization length scale <italic>k</italic>. The parameter <inline-formula id="ieqn-69"><mml:math id="mml-ieqn-69"><mml:mi>A</mml:mi></mml:math></inline-formula>, defined as <inline-formula id="ieqn-70"><mml:math id="mml-ieqn-70"><mml:mfrac><mml:mn>128</mml:mn><mml:mrow><mml:mn>27</mml:mn><mml:mi>&#x03C0;</mml:mi><mml:mrow><mml:mo>(</mml:mo><mml:mn>1</mml:mn><mml:mo>&#x2212;</mml:mo><mml:msup><mml:mi>&#x03BD;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup><mml:mo>)</mml:mo></mml:mrow><mml:mi>ln</mml:mi><mml:mo>&#x2061;</mml:mo><mml:mn>4</mml:mn></mml:mrow></mml:mfrac></mml:math></inline-formula> (plane strain) or <inline-formula id="ieqn-71"><mml:math id="mml-ieqn-71"><mml:mfrac><mml:mn>128</mml:mn><mml:mrow><mml:mn>27</mml:mn><mml:mi>&#x03C0;</mml:mi><mml:mi>ln</mml:mi><mml:mo>&#x2061;</mml:mo><mml:mn>4</mml:mn></mml:mrow></mml:mfrac></mml:math></inline-formula> (plane stress), aligns the crack-tip stress field with classical linear elastic fracture mechanics. The parameter <inline-formula id="ieqn-72"><mml:math id="mml-ieqn-72"><mml:mi>B</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mrow><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:mi>A</mml:mi><mml:msup><mml:mi>k</mml:mi><mml:mrow><mml:mo>&#x2217;</mml:mo></mml:mrow></mml:msup></mml:mrow><mml:mi>k</mml:mi></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, where <inline-formula id="ieqn-73"><mml:math id="mml-ieqn-73"><mml:msup><mml:mi>k</mml:mi><mml:mrow><mml:mo>&#x2217;</mml:mo></mml:mrow></mml:msup><mml:mo>=</mml:mo><mml:mfrac><mml:mrow><mml:mn>27</mml:mn><mml:mi>E</mml:mi><mml:msub><mml:mi>G</mml:mi><mml:mrow><mml:mi>c</mml:mi></mml:mrow></mml:msub></mml:mrow><mml:mrow><mml:mn>512</mml:mn><mml:msubsup><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>s</mml:mi></mml:mrow><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msubsup></mml:mrow></mml:mfrac></mml:math></inline-formula>, ensures energy consistency across diffusive crack regions while preserving material-specific strength dependencies. This approach eliminates <italic>k</italic>-driven artifacts, enabling robust predictions of crack paths in heterogeneous systems, particularly for the crack deflection at the GBs in multi-phase materials.</p>
<p>Expanding the energy framework, Zhen et al. [<xref ref-type="bibr" rid="ref-56">56</xref>] developed a thermodynamically consistent non-isothermal fracture phase field model through rigorous derivation of the Helmholtz free energy function and dissipation inequalities from non-equilibrium thermodynamics. The intricate coupling effects among crack propagation, MT and thermal conduction was well reflected by such a model. This approach provides a comprehensive framework for probing spatiotemporal evolution of multi-physics interactions under thermo-mechanical coupling. Zhu et al. [<xref ref-type="bibr" rid="ref-57">57</xref>] advanced the models of Zhao et al. [<xref ref-type="bibr" rid="ref-29">29</xref>] and Zhu and Luo [<xref ref-type="bibr" rid="ref-30">30</xref>] with four key enhancements, i.e., a temperature-dependent free energy functional, the differentiation of interfacial energy between different phases, an extra GB constraint energy terms, and a single-well potential phase field method, ultimately constructing a multi-mechanism coupled fracture phase field model for tetragonal zirconia polycrystals (TZPs).</p>
<p>Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-58">58</xref>] unified the Ginzburg-Landau theory of MT with variational principles of brittle fracture, establishing a multiphysics fracture phase field model for TZPs. This model accurately captured two dominant fracture mechanisms, i.e., secondary crack nucleation and propagation before main crack propagation, and crack branching. Significantly, Lotfolahpour et al. [<xref ref-type="bibr" rid="ref-59">59</xref>] modified the chemical free energy term in the fracture phase field model to ensure physically consistent elastic responses before the MT onset, enabling predictions of realistic mechanical behavior and experimentally observed microstructures. Pang et al. [<xref ref-type="bibr" rid="ref-60">60</xref>] developed a multiphase phase field model for thermal-shock fracture in multilayered ceramics, incorporating temperature-dependent material properties and the residual stresses caused by MT. The simulations accurately replicated the crack deflection induced by compressive stress redistribution during thermal shock, establishing a reference standard for ceramic thermal shock failure analysis. Xiong et al. [<xref ref-type="bibr" rid="ref-61">61</xref>] pioneered the coupling of crystal plasticity theory (encompassing dislocation slip, deformation twinning, and GB plasticity) with the fracture phase field model to dynamically capture the interplay between crack propagation and microstructural evolution in the NiTi SMAs under cyclic loading. They further formulated the non-isothermal thermo-mechanical coupling equations to simulate the latent heat effect on the dynamic crack propagation [<xref ref-type="bibr" rid="ref-61">61</xref>]. By introducing a GB energy function, they quantitatively characterized the GB suppression of MT and elucidated the role of grain refinement in modulating crack propagation rates and fracture modes (transgranular &#x2192; intergranular) [<xref ref-type="bibr" rid="ref-61">61</xref>].</p>
<p>The groundbreaking progress in three-dimensional (3D) fracture modeling has been achieved through the phase field method. Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-62">62</xref>] integrated variational principles for brittle fracture with MT dynamics governed by Ginzburg-Landau equations, establishing a 3D phase field model that successfully revealed the microscopic fracture mechanisms of SMCs. Clayton and Knap [<xref ref-type="bibr" rid="ref-63">63</xref>] derived the governing equations for quasi-static loading using variational methods and incorporated the anisotropic fracture surface energy within a 3D framework, enabling directional crack propagation along low-energy cleavage planes. Their simulations demonstrated that the fracture velocity increased when the fracture energy equaled twin boundary energy, while the twin-induced crack propagation decelerated when the fracture energy significantly exceeds the twin boundary energy. Xiong et al. [<xref ref-type="bibr" rid="ref-64">64</xref>] developed a 3D non-isothermal fracture phase field model for polycrystalline NiTi SMAs, which could reflect the crack propagation-MT interaction mechanisms. Numerical results verified the model&#x2019;s capability to reasonably predict the MT evolution, temperature distribution, and multi-field coupling during crack propagation under varying grain sizes (GSs) and loading rates, providing critical theoretical guidance for SMA engineering applications.</p>
<p>The variational principles for multi-physics coupling have been continued to refine. Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-65">65</xref>] developed a coupled variational framework for MT and brittle fracture, analyzing the tetragonal-to-monoclinic MT during the crack propagation in single-crystal zirconia. Their follow-up work [<xref ref-type="bibr" rid="ref-66">66</xref>] optimized the computational efficiency of the fracture phase field model, enhancing the predictions of crack initiation and propagation. These studies demonstrated the critical role of MT in fracture toughening and crack path selection. The validation of unconventional crack trajectories reinforced the importance of MT mechanisms in brittle fracture analysis. Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-58">58</xref>] coupled MT dynamics with brittle fracture variational theory, constructing a multi-physics model for TZPs. By introducing a GB energy dissipation tensor, the model resolved the competition between MT-induced microcracks and main crack propagation. Farahani et al. [<xref ref-type="bibr" rid="ref-67">67</xref>] developed a strongly coupled system of TDGL equations and mechanical equilibrium from micro-elasticity theory. The innovation lies in introducing a damage tensor as a mesoscale link between MT and fracture, enabling direct observation of energy dissipation mechanisms during MT.</p>
<p>In finite-strain modeling, Hasan et al. [<xref ref-type="bibr" rid="ref-68">68</xref>] innovatively integrated Hencky strain measures with objective rate tensors to develop an advanced fracture phase field model for the thermomechanical fracture in SMAs. This model could reflect the MT and reorientation of martensite variants initiating from a self-accommodated state. However, it is currently limited to quasi-static mechanical loading (neglecting latent heat effects) and slow thermal conduction (with weakened thermal gradient assumptions), highlighting critical directions for future research. In the future, the phase field models for the fracture behaviors of SMAs and SMCs still needs to be further improved and developed.</p>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>Phase Field Simulations of Fracture Behavior in SMAs</title>
<p>The unique MT characteristics of SMAs have demonstrated significant application potential in civil engineering [<xref ref-type="bibr" rid="ref-69">69</xref>], aerospace [<xref ref-type="bibr" rid="ref-70">70</xref>,<xref ref-type="bibr" rid="ref-71">71</xref>] and biomedical applications [<xref ref-type="bibr" rid="ref-72">72</xref>,<xref ref-type="bibr" rid="ref-73">73</xref>]. However, the complex mechanical behaviors during the MT pose critical challenges to material performance [<xref ref-type="bibr" rid="ref-74">74</xref>,<xref ref-type="bibr" rid="ref-75">75</xref>]. Recent investigations have revealed that the MT regions often develop residual stress fields and microstructural defects due to incomplete MT and multi-variant martensite coexistence [<xref ref-type="bibr" rid="ref-76">76</xref>]. These microstructural defects not only deteriorate mechanical properties but also act as nucleation sites for macrocracks, leading to premature failure.</p>
<p>To overcome these limitations, the phase field method has emerged as a powerful numerical tool for studying the fracture behavior of SMAs, owing to its inherent advantages in multi-physics coupling. This section will systematically review recent advances in phase field applications for the fracture behavior of SMAs, focusing on the factors affecting crack extension, including crystallographic orientation and grain size, as well as the fatigue fracture.</p>
<sec id="s3_1">
<label>3.1</label>
<title>Fracture Behavior of Single-Crystal SMAs: Effect of Crystallographic Orientation</title>
<p>The fracture behavior single crystal SMAs that is relatively easy to handle has attracted attention first. Relevant phase field studies have discussed the influence law of crystallographic orientation on the fracture behavior and the underlying mechanism. Ciss&#x00E9; and Zaeem [<xref ref-type="bibr" rid="ref-77">77</xref>] investigated the influence of crystallographic orientation on the crack tip toughening in CuAlBe SMAs through phase field simulations. Their study revealed a strong correlation between MT-induced toughening and the orientation angle of single-crystal SMAs (i.e., <inline-formula id="ieqn-74"><mml:math id="mml-ieqn-74"><mml:mi>&#x03B8;</mml:mi></mml:math></inline-formula> &#x003D; <inline-formula id="ieqn-75"><mml:math id="mml-ieqn-75"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-76"><mml:math id="mml-ieqn-76"><mml:msup><mml:mn>15</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-77"><mml:math id="mml-ieqn-77"><mml:msup><mml:mn>30</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-78"><mml:math id="mml-ieqn-78"><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-79"><mml:math id="mml-ieqn-79"><mml:msup><mml:mn>60</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-80"><mml:math id="mml-ieqn-80"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, and the corresponding systems are denoted as SC0, SC15, SC30, SC45, SC60, SC90, respectively). As shown in <xref ref-type="fig" rid="fig-1">Fig. 1</xref>, the elastic stiffness of the system exhibits a nonlinear dependence on <inline-formula id="ieqn-81"><mml:math id="mml-ieqn-81"><mml:mi>&#x03B8;</mml:mi></mml:math></inline-formula>, i.e., the stiffness increases monotonically from <inline-formula id="ieqn-82"><mml:math id="mml-ieqn-82"><mml:mi>&#x03B8;</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> to <inline-formula id="ieqn-83"><mml:math id="mml-ieqn-83"><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, then decreases gradually for <inline-formula id="ieqn-84"><mml:math id="mml-ieqn-84"><mml:mi>&#x03B8;</mml:mi><mml:mo>&#x003E;</mml:mo><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>. Notably, due to the intrinsic material symmetry constraints, SC30 and SC60 systems (as well as SC0 and SC90) display identical elastic responses. Further analysis demonstrated that the <inline-formula id="ieqn-85"><mml:math id="mml-ieqn-85"><mml:mi>&#x03B8;</mml:mi></mml:math></inline-formula> influences the toughening efficacy by governing the geometric configuration of stress-induced martensite wings and critical transformation stress thresholds. At specific orientations (e.g., SC15), the MT-induced stress redistribution shifts high-stress zones away from crack tips, enhancing the fracture toughness. Conversely, high-symmetry orientations (e.g., SC90) exhibit weakened toughening effects due to limited transformation strains along the loading directions.</p>
<fig id="fig-1">
<label>Figure 1</label>
<caption>
<title>Load-displacement curves for varying crystallographic orientations in CuAlBe SMAs (Cited from Ciss&#x00E9; and Zaeem [<xref ref-type="bibr" rid="ref-77">77</xref>]). Right panels show the martensite microstructures (<inline-formula id="ieqn-86"><mml:math id="mml-ieqn-86"><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>) near notch tips, with V1 (green), V2 (red), and austenite (blue)</title>
</caption>
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</fig>
<p>Xiong et al. [<xref ref-type="bibr" rid="ref-78">78</xref>] employed phase field simulations to study the crack propagation and MT-induced toughening in the single-crystal NiTi SMAs with varying crystallographic orientations (S0, S30, S45, S60, S90) and temperatures. The key findings include that: when the temperature exceeded the chemical equilibrium temperature (<inline-formula id="ieqn-87"><mml:math id="mml-ieqn-87"><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn>337.5</mml:mn><mml:mrow><mml:mtext>K</mml:mtext></mml:mrow></mml:math></inline-formula>), the MT toughening showed progressive weakening with rising temperature, whereas below <inline-formula id="ieqn-88"><mml:math id="mml-ieqn-88"><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>, the toughening capacity of martensite reorientation weakened as temperature decreased. To clarify the role of crystallographic orientation in MT toughening, this study focused on <inline-formula id="ieqn-89"><mml:math id="mml-ieqn-89"><mml:mi>T</mml:mi><mml:mo>=</mml:mo><mml:mn>360</mml:mn><mml:mrow><mml:mtext>K</mml:mtext></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mi>T</mml:mi><mml:mo>&#x003E;</mml:mo><mml:msub><mml:mi>T</mml:mi><mml:mrow><mml:mn>0</mml:mn></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and analyzed fracture behaviors across orientations (<xref ref-type="fig" rid="fig-2">Fig. 2</xref>). The simulations demonstrated that the MT-induced stress redistribution at crack tips effectively inhibited the crack propagation, with toughening effect strongly dependent on the crystallographic orientation. System S60 exhibited the highest average martensite fraction (<xref ref-type="fig" rid="fig-2">Fig. 2b</xref>) and the shortest crack length (<xref ref-type="fig" rid="fig-2">Fig. 2c</xref>), indicating superior stress relaxation capability. In contrast, systems S30 and S45, despite comparable martensite fractions, displayed significantly longer crack lengths than system S60, revealing that the extent of MT alone does not fully dictate toughening effectiveness.</p>
<fig id="fig-2">
<label>Figure 2</label>
<caption>
<title>Comparative simulation results for the single-crystal NiTi SMAs with different crystallographic orientations (Cited from Xiong et al. [<xref ref-type="bibr" rid="ref-78">78</xref>]): (<bold>a</bold>) Stress-displacement curves; (<bold>b</bold>) average martensite fraction vs. displacement; (<bold>c</bold>) crack length vs. displacement (excluding initial crack length, and full curves for non-MT systems omitted to highlight MT effects); (<bold>d</bold>) final martensite fraction and crack length post-loading</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-2.tif"/>
</fig>
</sec>
<sec id="s3_2">
<label>3.2</label>
<title>Fracture Behavior of Polycrystalline SMAs: Effect of Grain Size</title>
<p>Although the influence of crystallographic orientation on the fracture behavior of single-crystal SMAs has been simulated and discussed via phase field method (<xref ref-type="sec" rid="s3_1">Section 3.1</xref>), the SMAs in practical applications are almost all polycrystalline materials, whose fracture behaviors are quite different from those of single crystals and more complex. Therefore, the fracture behavior of polycrystalline SMAs has been addressed, and the effect of grain size has been given key consideration.</p>
<p>Using a 3D non-isothermal fracture phase field model, Xiong et al. [<xref ref-type="bibr" rid="ref-64">64</xref>] systematically investigated the synergistic effects of GS and loading rate on the crack propagation in polycrystalline NiTi SMAs. The study revealed that increasing GS significantly improves the peak stress (<xref ref-type="fig" rid="fig-3">Fig. 3a(i)</xref>) and fracture toughness while reducing the MT initiation stress (i.e., <inline-formula id="ieqn-90"><mml:math id="mml-ieqn-90"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mrow><mml:mtext>PT</mml:mtext></mml:mrow></mml:mrow></mml:msub></mml:math></inline-formula>, as shown in <xref ref-type="fig" rid="fig-3">Fig. 3a(ii)</xref>). The systems with larger GS (GS &#x2248; 100 nm) exhibited higher average martensite fractions (<xref ref-type="fig" rid="fig-3">Fig. 3a(iii)</xref>) and more pronounced temperature field evolution (<xref ref-type="fig" rid="fig-3">Fig. 3a(iv)</xref>), consistent with experimental observations of Ahadi and Sun [<xref ref-type="bibr" rid="ref-79">79</xref>]. <xref ref-type="fig" rid="fig-3">Fig. 3b</xref> compares microstructural morphologies of GS-60 and GS-15 systems before and after the marked decline in average martensite fraction-displacement curves. System GS-15 demonstrated longer uniform crack growth compared to System GS-60. As the GS decreases, the stress distribution at GBs becomes more homogeneous, favoring transgranular fracture. The study further discussed the GS-dependent fracture path transition, i.e., from the transgranular fracture (through grains) in fine-grained systems (GS &#x2248; 15 nm) to the intergranular fracture (along GBs) in coarse-grained systems (GS &#x2248; 100 nm). This transition arises from GB constraints on MT, i.e., grain refinement increases GB density, suppressing intragranular MT and reducing austenite-martensite interfaces, thereby homogenizing the MT. This mechanism aligns with GB-transformation interaction laws reported by Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-58">58</xref>].</p>
<fig id="fig-3">
<label>Figure 3</label>
<caption>
<title>Simulated crack propagation in polycrystalline NiTi SMAs with varying GSs under a loading rate of <inline-formula id="ieqn-91"><mml:math id="mml-ieqn-91"><mml:mrow><mml:mover><mml:mi>&#x03B5;</mml:mi><mml:mo>&#x02D9;</mml:mo></mml:mover></mml:mrow><mml:mo>=</mml:mo><mml:mn>0.01</mml:mn><mml:mspace width="thinmathspace" /><mml:msup><mml:mrow><mml:mtext>ns</mml:mtext></mml:mrow><mml:mrow><mml:mo>&#x2212;</mml:mo><mml:mn>1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> (Cited from Xiong et al. [<xref ref-type="bibr" rid="ref-64">64</xref>]). (<bold>a</bold>) Comparative results for systems GS-15, GS-60, and GS-100: (<bold>i</bold>) stress-displacement curves; (<bold>ii</bold>) maximum stress (<inline-formula id="ieqn-92"><mml:math id="mml-ieqn-92"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>m</mml:mi><mml:mi>a</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>) and MT initiation stress (<inline-formula id="ieqn-93"><mml:math id="mml-ieqn-93"><mml:msub><mml:mi>&#x03C3;</mml:mi><mml:mrow><mml:mi>P</mml:mi><mml:mi>T</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>); (<bold>iii</bold>) average martensite fraction vs. displacement, and (<bold>iv</bold>) temperature vs. displacement. (<bold>b</bold>) Microstructures of systems GS-60 and GS-15 before and after significant drops in martensite fraction-displacement curves. The 0 in the legend represents austenite, and 1, 2, 3 represent different martensite variants</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-3.tif"/>
</fig>
<p>Xiong et al. [<xref ref-type="bibr" rid="ref-61">61</xref>] further quantified the GS effects on the dislocation resistance, elucidating how grain refinement reduces the crack propagation rates and shifts fracture modes from intergranular to transgranular. For superelastic (SE) NiTi SMA (<xref ref-type="fig" rid="fig-4">Fig. 4a</xref>), increasing GS markedly elevates crack propagation rates (i.e., <inline-formula id="ieqn-94"><mml:math id="mml-ieqn-94"><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>a</mml:mi><mml:mrow><mml:mo>/</mml:mo></mml:mrow><mml:mrow><mml:mtext>d</mml:mtext></mml:mrow><mml:mi>N</mml:mi></mml:math></inline-formula>, <xref ref-type="fig" rid="fig-4">Fig. 4a(iv)</xref>), with fracture transitioning from transgranular (GS &#x2248; 20 nm) to intergranular (GS &#x2248; 100 nm) (<xref ref-type="fig" rid="fig-4">Fig. 4a(i&#x2013;iii)</xref>). In shape memory (SM) NiTi SMA (<xref ref-type="fig" rid="fig-4">Fig. 4b</xref>), the crack propagation rates remain GS-independent (<xref ref-type="fig" rid="fig-4">Fig. 4b(iv)</xref>) and slightly lower than the SE systems, with crack paths unaffected by GBs (<xref ref-type="fig" rid="fig-4">Fig. 4b(i&#x2013;iii)</xref>). This disparity stems from distinct energy dissipation mechanisms, i.e., the SE systems dissipate energy via reverse MT and plastic deformation (weakening toughening upon unloading), while the SM systems primarily dissipate energy through MR, avoiding reverse MT interference and achieving more effective dissipation.</p>
<fig id="fig-4">
<label>Figure 4</label>
<caption>
<title>Crack propagation behavior and growth rates (d<italic>a</italic>/d<italic>N</italic>) in superelastic (SE) and shape memory (SM) NiTi SMAs after five loading cycles (Cited from Xiong et al. [<xref ref-type="bibr" rid="ref-61">61</xref>]). (<bold>a</bold>) SE system: (<bold>i</bold>&#x2013;<bold>iii</bold>) crack microstructures for GS20, GS60, and GS100; (<bold>b</bold>) SM system: (<bold>i</bold>&#x2013;<bold>iii</bold>) crack microstructures for GS20, GS60, and GS100. V1, V3, and V5 denote martensite variants 1, 3, and 5.</title>
</caption>
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</fig>
</sec>
<sec id="s3_3">
<label>3.3</label>
<title>Fatigue Fracture of SMAs</title>
<p>Fracture behavior in SMAs occurs not only under short-term overload conditions but also poses significant risks in high-cycle and ultrahigh-cycle fatigue regimes. As an advanced fracture mechanics methodology, the phase field method provides a multiscale computational framework for fatigue damage evolution analysis. By coupling the MT thermodynamic principle with continuum damage theory, the phase field method enables accurate simulations of crack propagation under cyclic loading, establishing a theoretical foundation for fatigue life prediction and structural optimization in engineering components.</p>
<p>Simoes et al. [<xref ref-type="bibr" rid="ref-50">50</xref>] systematically investigated the key characteristics of fatigue fracture through phase field method across four representative cases: (i) the relationship between uniaxial tensile strain amplitude (<inline-formula id="ieqn-95"><mml:math id="mml-ieqn-95"><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:mi>&#x03B5;</mml:mi></mml:math></inline-formula>) and failure cycle number (<inline-formula id="ieqn-96"><mml:math id="mml-ieqn-96"><mml:mi>N</mml:mi></mml:math></inline-formula>) for smooth specimens (<xref ref-type="fig" rid="fig-5">Fig. 5a</xref>); (ii) fatigue crack propagation rates in single-edge notched specimens (<xref ref-type="fig" rid="fig-5">Fig. 5b</xref>); (iii) quantitative characterization of crack propagation rates based on Paris law (<xref ref-type="fig" rid="fig-5">Fig. 5c</xref>).</p>
<fig id="fig-5">
<label>Figure 5</label>
<caption>
<title>Phase field case studies on the fatigue fracture behavior of SMAs (Cited from Simoes et al. [<xref ref-type="bibr" rid="ref-50">50</xref>]): (<bold>a</bold>) Virtual <inline-formula id="ieqn-97"><mml:math id="mml-ieqn-97"><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:mi>&#x03B5;</mml:mi><mml:mo>&#x2212;</mml:mo><mml:mi>N</mml:mi></mml:math></inline-formula> curves for three material behaviors, with strain range <inline-formula id="ieqn-98"><mml:math id="mml-ieqn-98"><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:mi>&#x03B5;</mml:mi></mml:math></inline-formula> normalized by critical strain; (<bold>b</bold>) cracked square plate showing constitutive model effects on crack density evolution (AT1 vs. AT2 formulations) under displacement-controlled cyclic loading: (<bold>i</bold>) <inline-formula id="ieqn-99"><mml:math id="mml-ieqn-99"><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x221E;</mml:mi></mml:mrow></mml:msup><mml:mo>=</mml:mo><mml:mn>0.016</mml:mn><mml:mtext>&#x00A0;</mml:mtext><mml:mrow><mml:mtext>mm</mml:mtext></mml:mrow></mml:math></inline-formula>, (<bold>ii</bold>) <inline-formula id="ieqn-100"><mml:math id="mml-ieqn-100"><mml:mrow><mml:mi mathvariant="normal">&#x0394;</mml:mi></mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mi mathvariant="normal">&#x221E;</mml:mi></mml:mrow></mml:msup><mml:mo>=</mml:mo><mml:mn>0.012</mml:mn><mml:mtext>&#x00A0;</mml:mtext><mml:mrow><mml:mtext>mm</mml:mtext></mml:mrow></mml:math></inline-formula>; (<bold>c</bold>) boundary layer model for Paris law-based crack propagation: (<bold>i</bold>) schematic of boundary layer structure with small transformation zone assumption, (<bold>ii</bold>) crack propagation vs. cycle number under varying load ranges, and (<bold>iii</bold>) fatigue crack propagation rates vs. load ranges for three material behaviors</title>
</caption>
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</fig>
<p>In engineering applications, the multiscale phase field framework developed by Simoes and Mart&#x00ED;nez-Pa&#x00F1;eda [<xref ref-type="bibr" rid="ref-47">47</xref>] constitutes a significant advancement. This framework establishes a cross-scale coupling mechanism linking microscopic transformation to macroscopic damage mechanics, enabling full-domain fatigue life prediction for complex component geometries, multi-field boundary conditions, and nonlinear material parameters. This model has been validated by successfully simulating the fatigue fracture in biomedical stents (<xref ref-type="fig" rid="fig-6">Fig. 6</xref>).</p>
<fig id="fig-6">
<label>Figure 6</label>
<caption>
<title>Contours of phase field parameter <inline-formula id="ieqn-101"><mml:math id="mml-ieqn-101"><mml:mi>&#x03D5;</mml:mi></mml:math></inline-formula> in an SMA stent during systolic and diastolic cycles (compression-expansion) (Cited from Simoes and Mart&#x00ED;nez-Pa&#x00F1;eda [<xref ref-type="bibr" rid="ref-47">47</xref>])</title>
</caption>
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</fig>
</sec>
</sec>
<sec id="s4">
<label>4</label>
<title>Phase Field Simulations of Fracture Behavior in SMCs</title>
<p>SMCs have shown great potential for application in the field of automotive [<xref ref-type="bibr" rid="ref-80">80</xref>,<xref ref-type="bibr" rid="ref-81">81</xref>], additive manufacturing [<xref ref-type="bibr" rid="ref-82">82</xref>,<xref ref-type="bibr" rid="ref-83">83</xref>] and aerospace [<xref ref-type="bibr" rid="ref-84">84</xref>] with their unique MT appeal. Similarly, facing the influence of complex mechanical behavior on material properties during MT, it is still necessary to use the phase-field method, which has advantages in multi-physical field coupling. In the following section, a systematic review of recent advances in phase field simulation to the fracture behavior of SMCs is presented, focusing on the factors affecting the crack extension, including crystallographic orientation and grain boundary properties.</p>
<sec id="s4_1">
<label>4.1</label>
<title>Fracture Behavior of Single-Crystal SMCs: Effect of Crystallographic Orientation</title>
<p>Similar to SMAs, the fracture behavior single crystal SMAs that is relatively easy to handle has attracted attention first. The influence law of crystallographic orientation on the fracture behavior and the underlying mechanism have been discussed. Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-65">65</xref>] investigated the fracture mechanisms in the single-crystal tetragonal zirconia using an MT-coupled fracture phase field model. Their work demonstrated that the MT inhibited the crack propagation through energy dissipation processes, with crystallographic orientation playing a determinative role in crack path evolution and toughening. Comparative analyses of crack paths (<xref ref-type="fig" rid="fig-7">Fig. 7</xref>) and stress-strain curves (<xref ref-type="fig" rid="fig-8">Fig. 8</xref>) across orientations (<inline-formula id="ieqn-102"><mml:math id="mml-ieqn-102"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-103"><mml:math id="mml-ieqn-103"><mml:msup><mml:mn>20</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-104"><mml:math id="mml-ieqn-104"><mml:msup><mml:mn>50</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-105"><mml:math id="mml-ieqn-105"><mml:msup><mml:mn>60</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-106"><mml:math id="mml-ieqn-106"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>) revealed pronounced orientation-dependent fracture characteristics. At <inline-formula id="ieqn-107"><mml:math id="mml-ieqn-107"><mml:msup><mml:mn>50</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, the crack paths exhibited significant deflection (<xref ref-type="fig" rid="fig-7">Fig. 7c</xref>), indicating optimal stress redistribution for toughening. In contrast, <inline-formula id="ieqn-108"><mml:math id="mml-ieqn-108"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation resulted in straight crack propagation (<xref ref-type="fig" rid="fig-7">Fig. 7e</xref>), with reduced toughening due to diminished stress redistribution. These findings align with critical stress differences in stress-strain curves (<xref ref-type="fig" rid="fig-8">Fig. 8</xref>), i.e., <inline-formula id="ieqn-109"><mml:math id="mml-ieqn-109"><mml:msup><mml:mn>50</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation achieved the maximum critical stress, while <inline-formula id="ieqn-110"><mml:math id="mml-ieqn-110"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> showed the minimum one.</p>
<fig id="fig-7">
<label>Figure 7</label>
<caption>
<title>Effect of crystallographic orientation on crack propagation in a single-crystal tetragonal zirconia under Mode-I loading (Cited from Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-65">65</xref>]). Left and right columns show synchronized MT and crack evolution at 600 s and 3500 s, respectively</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-7.tif"/>
</fig><fig id="fig-8">
<label>Figure 8</label>
<caption>
<title>Stress-strain curves during the crack propagation in the single-crystal tetragonal zirconia with varying crystallographic orientations (Cited from Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-65">65</xref>]). The loading rates and simulation times were consistent. The maximum and minimum toughening occurred at <inline-formula id="ieqn-111"><mml:math id="mml-ieqn-111"><mml:msup><mml:mn>50</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> and <inline-formula id="ieqn-112"><mml:math id="mml-ieqn-112"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, respectively</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-8.tif"/>
</fig>
<p>Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-62">62</xref>] systematically investigated the MT behavior of tetragonal zirconia under mechanical loading and its influence on the fracture behavior by incorporating 12 monoclinic martensite variants into a fracture phase field model. The numerical simulations successfully replicated the experimentally observed features, including surface morphology uplift, formation of self-accommodated martensite pairs, and phase zone fragmentation. A systematic analysis of crystallographic orientation effect (<xref ref-type="fig" rid="fig-9">Fig. 9</xref>) revealed that different crystallographic orientations critically regulate monoclinic variant evolution and crack propagation modes. At <inline-formula id="ieqn-113"><mml:math id="mml-ieqn-113"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation, only <italic>ABC</italic> and <italic>AB</italic><inline-formula id="ieqn-114"><mml:math id="mml-ieqn-114"><mml:mspace width="negativethinmathspace" /><mml:mrow><mml:mover><mml:mi>C</mml:mi><mml:mo stretchy="false">&#x00AF;</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula> martensite variants were formed, with cracks propagating uniformly through the thickness. For <inline-formula id="ieqn-115"><mml:math id="mml-ieqn-115"><mml:msup><mml:mn>15</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation, while the same variants (<italic>ABC</italic> and <italic>ABC&#x0304;</italic>) persisted, the crack propagation transitioned to a non-uniform pattern. When the orientation angle increased to <inline-formula id="ieqn-116"><mml:math id="mml-ieqn-116"><mml:msup><mml:mn>30</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, four distinct variants (<italic>ABC</italic>, <italic>AB</italic><inline-formula id="ieqn-117"><mml:math id="mml-ieqn-117"><mml:mspace width="negativethinmathspace" /><mml:mrow><mml:mover><mml:mi>C</mml:mi><mml:mo stretchy="false">&#x00AF;</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula>, <italic>BAC</italic>, <italic>BA</italic><inline-formula id="ieqn-118"><mml:math id="mml-ieqn-118"><mml:mspace width="negativethinmathspace" /><mml:mrow><mml:mover><mml:mi>C</mml:mi><mml:mo stretchy="false">&#x00AF;</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula>) emerged, accompanied by significant spatial heterogeneity in variant distributions. This orientation-dependent transformation mechanism highlights how the crystallographic orientation governs the stress redistribution at crack tips by modifying the MT driving forces.</p>
<fig id="fig-9">
<label>Figure 9</label>
<caption>
<title>Martensite microstructures and crack patterns at <inline-formula id="ieqn-121"><mml:math id="mml-ieqn-121"><mml:mi>t</mml:mi><mml:mo>=</mml:mo><mml:mn>200</mml:mn><mml:mtext>&#x00A0;</mml:mtext><mml:mrow><mml:mtext>s</mml:mtext></mml:mrow></mml:math></inline-formula> and <inline-formula id="ieqn-122"><mml:math id="mml-ieqn-122"><mml:mn>2000</mml:mn><mml:mtext>&#x00A0;</mml:mtext><mml:mrow><mml:mtext>s</mml:mtext></mml:mrow></mml:math></inline-formula> for the orientation angles of <inline-formula id="ieqn-123"><mml:math id="mml-ieqn-123"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-124"><mml:math id="mml-ieqn-124"><mml:msup><mml:mn>15</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-125"><mml:math id="mml-ieqn-125"><mml:msup><mml:mn>30</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-126"><mml:math id="mml-ieqn-126"><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-127"><mml:math id="mml-ieqn-127"><mml:msup><mml:mn>60</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, <inline-formula id="ieqn-128"><mml:math id="mml-ieqn-128"><mml:msup><mml:mn>75</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, and <inline-formula id="ieqn-129"><mml:math id="mml-ieqn-129"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> (Cited from Moshkelgosha and Mamivand [<xref ref-type="bibr" rid="ref-62">62</xref>])</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-9.tif"/>
</fig>
<p>Sun et al. [<xref ref-type="bibr" rid="ref-85">85</xref>] investigated the ferroelastic toughening mechanisms in yttria-stabilized zirconia single crystals under varying crystallographic orientations using a coupled fracture phase field model. The study revealed that at <inline-formula id="ieqn-119"><mml:math id="mml-ieqn-119"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation (<italic>c</italic>-axis parallel to the crack surface), the needle-like ferroelastic domain switching structures formed symmetrically ahead of the crack tip (<xref ref-type="fig" rid="fig-10">Fig. 10a</xref>). These domains grew along approximately <inline-formula id="ieqn-120"><mml:math id="mml-ieqn-120"><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> directions, with new domains continuously nucleating ahead of the advancing crack. Existing domains behind the crack tip gradually recovered through reverse switching due to the stress relaxation. This demonstrated that the stress concentration at the crack front drove the domain switching, whereas stress relaxation in the crack wake promoted the domain recovery.</p>
<fig id="fig-10">
<label>Figure 10</label>
<caption>
<title>Ferroelastic domain evolution in yttria-stabilized zirconia single crystals under varying crystallographic orientations and loading modes (Cited from Sun et al. [<xref ref-type="bibr" rid="ref-85">85</xref>]): (<bold>a</bold>) Domain switching under Load I at <inline-formula id="ieqn-130"><mml:math id="mml-ieqn-130"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation; (<bold>b</bold>) Load I at <inline-formula id="ieqn-131"><mml:math id="mml-ieqn-131"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation; (<bold>c</bold>) Load II at <inline-formula id="ieqn-132"><mml:math id="mml-ieqn-132"><mml:msup><mml:mn>0</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation; (<bold>d</bold>) Load II at <inline-formula id="ieqn-133"><mml:math id="mml-ieqn-133"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation; (<bold>e</bold>) Load I at <inline-formula id="ieqn-134"><mml:math id="mml-ieqn-134"><mml:msup><mml:mn>60</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation. Left and right columns show initial crack growth and propagation to 1.0 &#x03BC;m, respectively</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-10.tif"/>
</fig>
<p>At <inline-formula id="ieqn-135"><mml:math id="mml-ieqn-135"><mml:msup><mml:mn>90</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> orientation (<italic>c</italic>-axis perpendicular to the crack surface), the ferroelastic domains clustered behind the crack tip, forming needle-like morphologies aligned perpendicular to the crack plane (<xref ref-type="fig" rid="fig-10">Fig. 10b</xref>). This spatial distribution aligns with stress field patterns reported by Wang et al. [<xref ref-type="bibr" rid="ref-86">86</xref>] and Sluka et al. [<xref ref-type="bibr" rid="ref-87">87</xref>], i.e., the residual stresses behind the crack maintained domain switching, while the stress concentrations ahead were insufficient to trigger domain switching. For intermediate orientations (e.g., <inline-formula id="ieqn-136"><mml:math id="mml-ieqn-136"><mml:msup><mml:mn>60</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>), the domain switching localized predominantly on the left side of the crack (<xref ref-type="fig" rid="fig-10">Fig. 10e</xref>), resulting in a rightward deflection of the crack path. This asymmetric evolution directly correlates with orientation-dependent stress redistribution, demonstrating that crystallographic orientation effectively modulates the crack propagation paths.</p>
</sec>
<sec id="s4_2">
<label>4.2</label>
<title>Fracture Behavior of Polycrystalline SMCs: Effect of Grain Boundary Properties</title>
<p>Compared with the single-crystal system, there are a large number of grain boundaries in the polycrystalline system, which may affect the fracture behavior of SMCs. Therefore, some researchers have studied the influence of grain boundary properties on the fracture behavior of SMCs through phase field simulation. Zhu and Luo [<xref ref-type="bibr" rid="ref-30">30</xref>] investigated the low-temperature degradation phenomena in yttria-stabilized TZPs under humid environments using a fracture phase field model to simulate the tetragonal-to-monoclinic MT and GB-induced microcrack evolution. The study focused on the influence of martensite variant width and incidence angles on the microcrack nucleation. The simulation results demonstrated that varying incidence angles could significantly influence the crack initiation/propagation modes and govern the microstructure of monoclinic variant and intergranular microcrack distributions. In the subsequent work, Zhu et al. [<xref ref-type="bibr" rid="ref-57">57</xref>] revealed how relative fracture toughness differences between GBs and the matrix influence the crack paths and toughening mechanisms (<xref ref-type="fig" rid="fig-11">Fig. 11</xref>). For the &#x201C;strong GBs&#x201D; (the fracture toughness &#x003D; 1.2 MPa&#x00B7;m1/2, matching the matrix), the cracks required higher external loads (180 MPa) to propagate (<xref ref-type="fig" rid="fig-11">Fig. 11a</xref>). For the &#x201C;weak GBs&#x201D; (the fracture toughness &#x003D; 0.5 MPa&#x00B7;m1/2), the cracks propagated along the GBs under 150&#x2013;170 MPa (<xref ref-type="fig" rid="fig-11">Fig. 11b</xref>,<xref ref-type="fig" rid="fig-11">f</xref>). The stress concentration at monoclinic variant-GB interfaces triggered intergranular microcrack nucleation (<xref ref-type="fig" rid="fig-11">Fig. 11b</xref>), while the interactions between main cracks and microcracks led to crack deflection along GBs via a healing-reinitiation dynamic process (<xref ref-type="fig" rid="fig-11">Fig. 11f</xref>). The GB orientation effects were further elucidated through polycrystalline orientation adjustments (Orientation II, <xref ref-type="fig" rid="fig-11">Fig. 11c</xref>,<xref ref-type="fig" rid="fig-11">d</xref>,<xref ref-type="fig" rid="fig-11">g</xref>,<xref ref-type="fig" rid="fig-11">h</xref>). The &#x201C;strong GBs&#x201D; promoted near-linear crack growth under specific orientations (<xref ref-type="fig" rid="fig-11">Fig. 11c</xref>,<xref ref-type="fig" rid="fig-11">g</xref>), whereas the &#x201C;weak GBs&#x201D; induced the interactions between main cracks and intergranular microcracks at triple junctions (<xref ref-type="fig" rid="fig-11">Fig. 11h</xref>), highlighting the role of GB topology in fracture mode regulation. Experimental validation confirmed that crack bifurcation (<xref ref-type="fig" rid="fig-11">Fig. 11f</xref>), intergranular microcracks (<xref ref-type="fig" rid="fig-11">Fig. 11b</xref>), and healing phenomena (<xref ref-type="fig" rid="fig-11">Fig. 11f</xref>) align with observations in [<xref ref-type="bibr" rid="ref-88">88</xref>&#x2013;<xref ref-type="bibr" rid="ref-91">91</xref>], corroborating the reliability of the model.</p>
<fig id="fig-11">
<label>Figure 11</label>
<caption>
<title>MT and crack propagation in TZPs under varying GB strengths (fracture toughness), crystal properties, and orientations at Time 1 (onset of intergranular microcracks or significant crack path changes) and Time 2 (simulation termination) (Cited from Zhu et al. [<xref ref-type="bibr" rid="ref-57">57</xref>]). Order parameters (<inline-formula id="ieqn-148"><mml:math id="mml-ieqn-148"><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>1</mml:mn></mml:mrow></mml:msub><mml:mo>&#x2212;</mml:mo><mml:msub><mml:mi>&#x03B7;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula>) and crack phases are shown in magnified windows. Case 1: TZP with &#x201C;strong GBs&#x201D; (Orientation I) under sequential loading of 180 MPa and 170 MPa; Case 2: TZP with &#x201C;weak GBs&#x201D; (Orientation I) under 170 MPa; Case 3: TZP with &#x201C;strong GBs&#x201D; (Orientation II) under 150 MPa; Case 4: TZP with &#x201C;weak GBs&#x201D; (Orientation II) under 150 MPa</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-11.tif"/>
</fig>
<p>Emdadi and Zaeem [<xref ref-type="bibr" rid="ref-55">55</xref>] investigated the fracture behavior in ZrB2 bicrystals using a modified fracture phase field model. As shown in <xref ref-type="fig" rid="fig-12">Fig. 12a</xref>,<xref ref-type="fig" rid="fig-12">b</xref>, increasing misorientation angle <inline-formula id="ieqn-137"><mml:math id="mml-ieqn-137"><mml:msub><mml:mi>&#x03B8;</mml:mi><mml:mrow><mml:mn>2</mml:mn></mml:mrow></mml:msub></mml:math></inline-formula> (grain orientation difference) and decreasing GB angle <inline-formula id="ieqn-138"><mml:math id="mml-ieqn-138"><mml:mi>&#x03B1;</mml:mi></mml:math></inline-formula> under tensile loading strongly promoted intergranular crack propagation. At <inline-formula id="ieqn-139"><mml:math id="mml-ieqn-139"><mml:mi>&#x03B1;</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> (<xref ref-type="fig" rid="fig-12">Fig. 12a</xref>), the intergranular and transgranular propagation competed, i.e., the cracks prefer GBs below a critical strength threshold but penetrate grains for stronger GBs. Further studies [<xref ref-type="bibr" rid="ref-92">92</xref>] revealed the synergistic effects of <inline-formula id="ieqn-140"><mml:math id="mml-ieqn-140"><mml:mi>&#x03B1;</mml:mi></mml:math></inline-formula> and <inline-formula id="ieqn-141"><mml:math id="mml-ieqn-141"><mml:msub><mml:mi>&#x03B8;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula> (<xref ref-type="fig" rid="fig-12">Fig. 12c</xref>,<xref ref-type="fig" rid="fig-12">d</xref>). For a fixed <inline-formula id="ieqn-142"><mml:math id="mml-ieqn-142"><mml:mi>&#x03B1;</mml:mi></mml:math></inline-formula>, the intergranular fracture tendency increases with <inline-formula id="ieqn-143"><mml:math id="mml-ieqn-143"><mml:msub><mml:mi>&#x03B8;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>, and reducing <inline-formula id="ieqn-144"><mml:math id="mml-ieqn-144"><mml:mi>&#x03B1;</mml:mi></mml:math></inline-formula> (aligning initial cracks with GBs) raises the critical GB strength required for intergranular propagation. Specifically, at <inline-formula id="ieqn-145"><mml:math id="mml-ieqn-145"><mml:mi>&#x03B1;</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mn>40</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula>, the critical GB strength threshold exceeds that at <inline-formula id="ieqn-146"><mml:math id="mml-ieqn-146"><mml:mi>&#x03B1;</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mn>50</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> for identical <inline-formula id="ieqn-147"><mml:math id="mml-ieqn-147"><mml:msub><mml:mi>&#x03B8;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>, indicating that the GB geometric alignment enhances the crack resistance. This orientation-strength triadic coupling provides theoretical guidance for polycrystalline microstructure design.</p>
<fig id="fig-12">
<label>Figure 12</label>
<caption>
<title>Relationships between crack propagation, grain misorientation, GB angle, and GB strength (Cited from Emdadi and Zaeem [<xref ref-type="bibr" rid="ref-55">55</xref>]). (<bold>a</bold>,<bold>b</bold>) Crack propagation in the bicrystal under varying grain misorientation angles (<inline-formula id="ieqn-149"><mml:math id="mml-ieqn-149"><mml:mi>&#x03B8;</mml:mi></mml:math></inline-formula>) and GB angles (<inline-formula id="ieqn-150"><mml:math id="mml-ieqn-150"><mml:mi>&#x03B1;</mml:mi></mml:math></inline-formula>); (<bold>c</bold>) critical GB strength (<inline-formula id="ieqn-151"><mml:math id="mml-ieqn-151"><mml:mi>&#x03C7;</mml:mi></mml:math></inline-formula>) for intergranular cracking vs. misorientation angle (<inline-formula id="ieqn-152"><mml:math id="mml-ieqn-152"><mml:msub><mml:mi>&#x03B8;</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:math></inline-formula>) at different GB angles (<inline-formula id="ieqn-153"><mml:math id="mml-ieqn-153"><mml:mi>&#x03B1;</mml:mi></mml:math></inline-formula>); (<bold>d</bold>) intergranular/transgranular crack regimes vs. GB strength at <inline-formula id="ieqn-154"><mml:math id="mml-ieqn-154"><mml:mi>&#x03B1;</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mn>45</mml:mn><mml:mrow><mml:mo>&#x2218;</mml:mo></mml:mrow></mml:msup></mml:math></inline-formula> (<inline-formula id="ieqn-155"><mml:math id="mml-ieqn-155"><mml:msubsup><mml:mrow><mml:mtext>G</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>c</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mtext>GB</mml:mtext></mml:mrow></mml:mrow></mml:msubsup><mml:mo>=</mml:mo><mml:msubsup><mml:mrow><mml:mtext>G</mml:mtext></mml:mrow><mml:mrow><mml:mrow><mml:mtext>c</mml:mtext></mml:mrow></mml:mrow><mml:mrow><mml:mrow><mml:mtext>bulk</mml:mtext></mml:mrow></mml:mrow></mml:msubsup></mml:math></inline-formula>)</title>
</caption>
<graphic mimetype="image" mime-subtype="tif" xlink:href="CMC_68226-fig-12.tif"/>
</fig>
</sec>
</sec>
<sec id="s5">
<label>5</label>
<title>Summary and Outlook</title>
<sec id="s5_1">
<label>5.1</label>
<title>Summary</title>
<p>The fracture phase field method, an advanced simulation approach integrating phase transformation theory and fracture mechanics, has demonstrated extensive applicability and powerful characterization capabilities in materials science. Based on energy variational principles, the fracture phase field method naturally incorporates crack initiation and propagation into material energy evolution, circumventing the challenges of crack interface tracking inherent in conventional models. By introducing continuous order parameters, the fracture phase field method simultaneously accounts for chemical free energy, elastic strain energy, and crack gradient energy, enabling effective simulation of coupled damage evolution, MT, and mechanical responses under external loads. This provides a reliable theoretical framework for elucidating intrinsic relationships between microstructures and macroscopic material properties.</p>
<p>Current fracture phase field studies on SMAs and SMCs mainly concentrate on two primary directions as follows:
<list list-type="simple">
<list-item><label>(1)</label>
<p>Theoretical advancements, including multi-physics coupling mechanisms, and the incorporation of various fracture criteria in the fracture phase field models for SMAs and SMCs.</p></list-item>
<list-item><label>(2)</label>
<p>The revelation of microscopic mechanisms, including the effects of crystallographic orientation, grain size, grain boundary, etc, on the fracture behaviors of SMAs and SMCs.</p></list-item>
</list></p>
<p>With advancements in computational capabilities, the fracture phase field method has become a fundamental tool in basic research and increasingly critical for failure prediction, high-performance material design, and engineering safety assessment of SMAs and SMCs.</p>
</sec>
<sec id="s5_2">
<label>5.2</label>
<title>Limitations and Challenges</title>
<p>So far, the literatures of phase field modeling of the fracture behaviors of SMAs and SMCs are very limited, and the related research direction is still in the early stage of progress. The phase field researches focusing on the fracture behaviors of SMAs and SMCs are not systematic enough, and their goals are relatively scattered. Therefore, it is difficult to compare the simulation results or research goals by discussing the roles of material parameters (e.g., fracture toughness, elastic anisotropy) taken from different literatures. Moreover, the setting of some empirical parameters (e.g., interface energy coefficient) in different literatures is not unified (this does not affect the rationality of qualitatively analyzing the simulation results and the conclusions drawn), which can lead to different mesh size settings (even several orders of magnitude different). The computational cost has not been mentioned in most of the relevant literatures. This makes it very difficult to evaluate the computational costs and mesh dependencies of different models through comparison.</p>
<p>Despite significant progress in the fracture behaviors of SMAs and SMCs, the fracture phase field method encounters several limitations in complex service environments. For example, systematic frameworks are lacking for modeling magnetic field-induced MT, hygrothermal effects, and corrosion/oxidation influences on crack evolution in SMAs or SMCs. Moreover, the existing fracture phase field models for SMAs and SMCs rely on quasi-static assumptions, failing to accurately capture dynamic fracture processes under high-velocity impacts. The predictive capability remains constrained for complex fracture modes, including mixed-mode II/III crack growth, multi-crack interactions, bifurcation, and self-healing. Modeling GB effects in polycrystalline SMAs and SMCs faces challenges in parameter selection and experimental validation, and the introducing of microstructural defects (e.g., interfaces, dislocations, vacancies) are insufficiently resolved. High computational costs and low numerical efficiency further hinder large-scale applications. Fatigue crack evolution modeling remains underdeveloped, with phase field frameworks of fatigue fracture of SMAs and SMCs requiring substantial refinement.</p>
<p>In the future, the fracture phase field research should focus on multi-physics coupled model development, scale-bridging innovations, and enhanced adaptability to complex environments. These advancements will address critical challenges in fracture toughness enhancement, structural performance optimization, and durability extension, particularly in aerospace and biomedical applications where model reliability directly impacts application performance. Critical research directions include development of fatigue-phase field, integration of macro-micro mechanisms, and practical engineering applications with improved computational efficiency. Only by achieving these goals can fracture phase field method transition from a research tool to an industry-reliable solution for addressing practical material failure challenges.</p>
</sec>
</sec>
</body>
<back>
<ack>
<p>Not applicable.</p>
</ack>
<sec>
<title>Funding Statement</title>
<p>This work is supported by the National Natural Science Foundation of China (12202294) and the Sichuan Science and Technology Program (2024NSFSC1346).</p>
</sec>
<sec>
<title>Author Contributions</title>
<p>Junhui Hua: Writing&#x2014;original draft, Investigation; Junyuan Xiong: Writing&#x2014;review &#x0026; editing; Bo Xu: Conceptualization, Writing&#x2014;review &#x0026; editing, Funding acquisition; Chong Wang: Validation, Supervision; Qingyuan Wang: Validation. All authors reviewed the results and approved the final version of the manuscript.</p>
</sec>
<sec sec-type="data-availability">
<title>Availability of Data and Materials</title>
<p>Not applicable.</p>
</sec>
<sec>
<title>Ethics Approval</title>
<p>Not applicable.</p>
</sec>
<sec sec-type="COI-statement">
<title>Conflicts of Interest</title>
<p>The authors declare no conflicts of interest to report regarding the present study.</p>
</sec>
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