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<article xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:oasis="http://docs.oasis-open.org/ns/oasis-exchange/table" xml:lang="en" dtd-version="3.0" article-type="research-article">
  <front>
    <journal-meta><journal-id journal-id-type="publisher">WES</journal-id><journal-title-group>
    <journal-title>Wind Energy Science</journal-title>
    <abbrev-journal-title abbrev-type="publisher">WES</abbrev-journal-title><abbrev-journal-title abbrev-type="nlm-ta">Wind Energ. Sci.</abbrev-journal-title>
  </journal-title-group><issn pub-type="epub">2366-7451</issn><publisher>
    <publisher-name>Copernicus Publications</publisher-name>
    <publisher-loc>Göttingen, Germany</publisher-loc>
  </publisher></journal-meta>
    <article-meta>
      <article-id pub-id-type="doi">10.5194/wes-8-1597-2023</article-id><title-group><article-title>OF<inline-formula><mml:math id="M1" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>: coupling OpenFAST and OpenFOAM for high-fidelity aero-hydro-servo-elastic FOWT simulations</article-title><alt-title>OF<inline-formula><mml:math id="M2" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>: coupling OpenFAST and OpenFOAM for FOWT simulations</alt-title>
      </title-group><?xmltex \runningtitle{OF${}^{2}$: coupling OpenFAST and OpenFOAM for FOWT simulations}?><?xmltex \runningauthor{G. Campaña-Alonso et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1 aff2">
          <name><surname>Campaña-Alonso</surname><given-names>Guillén</given-names></name>
          <email>gcampana@cener.com</email>
        <ext-link>https://orcid.org/0000-0002-5312-3069</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Martín-San-Román</surname><given-names>Raquel</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-0898-9058</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Méndez-López</surname><given-names>Beatriz</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Benito-Cia</surname><given-names>Pablo</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-9852-6120</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Azcona-Armendáriz</surname><given-names>José</given-names></name>
          
        </contrib>
        <aff id="aff1"><label>1</label><institution>Wind Energy Department, Centro Nacional de Energías Renovables (CENER),<?xmltex \hack{\break}?> Ciudad de la Innovación, 7, 31621 Sarriguren, Spain</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>UPM, E.T.S.I. Aeronáutica y del Espacio, Universidad Politécnica de Madrid,<?xmltex \hack{\break}?> Plaza Cardenal Cisneros, 3, 28040 Madrid, Spain</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Guillén Campaña-Alonso (gcampana@cener.com)</corresp></author-notes><pub-date><day>24</day><month>October</month><year>2023</year></pub-date>
      
      <volume>8</volume>
      <issue>10</issue>
      <fpage>1597</fpage><lpage>1611</lpage>
      <history>
        <date date-type="received"><day>15</day><month>February</month><year>2023</year></date>
           <date date-type="rev-request"><day>3</day><month>March</month><year>2023</year></date>
           <date date-type="rev-recd"><day>22</day><month>June</month><year>2023</year></date>
           <date date-type="accepted"><day>26</day><month>June</month><year>2023</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2023 Guillén Campaña-Alonso et al.</copyright-statement>
        <copyright-year>2023</copyright-year>
      <license license-type="open-access"><license-p>This work is licensed under the Creative Commons Attribution 4.0 International License. To view a copy of this licence, visit <ext-link ext-link-type="uri" xlink:href="https://creativecommons.org/licenses/by/4.0/">https://creativecommons.org/licenses/by/4.0/</ext-link></license-p></license></permissions><self-uri xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023.html">This article is available from https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023.html</self-uri><self-uri xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023.pdf">The full text article is available as a PDF file from https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023.pdf</self-uri>
      <abstract><title>Abstract</title>

      <p id="d1e145">The numerical study of floating offshore wind turbines (FOWTs) requires accurate integrated simulations which consider the aerodynamic, hydrodynamic, servo and elastic responses of these systems. In addition, the floating system dynamics couplings need to be included to  calculate the excitation over the ensemble accurately. In this paper, a new tool has been developed for coupling NREL's aero-servo-elastic tool OpenFAST with the computational fluid dynamics (CFD) toolbox OpenFOAM. OpenFAST is used to model the rotor aerodynamics along with the flexible response of the different components of the wind turbine and the controller at each time step considering the dynamic response of the platform. OpenFOAM is used to simulate the hydrodynamics and the platform's response considering the loads from the wind turbine. The whole simulation environment is called OF<inline-formula><mml:math id="M3" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> (OpenFAST and OpenFOAM). The OC4 DeepCWind semi-submersible FOWT together with NREL's 5 MW wind turbine has been simulated using OF<inline-formula><mml:math id="M4" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> under two load cases. The purpose of coupling these tools to simulate FOWT is to obtain high-fidelity results for design purposes, thereby reducing the computational time compared with the use of CFD simulations both for the rotor aerodynamics, which usually consider rigid blades, and for the platform's hydrodynamics. The OF<inline-formula><mml:math id="M5" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> approach also allows us to include the aero-servo-elastic couplings that exist on the wind turbine along with the hydrodynamic system resolved by CFD. High-complexity situations of floating offshore wind turbines, like storms, yaw drifts, weather vanes or mooring line breaks, which imply high displacements and rotations of the floating platform or relevant non-linear effects, can be resolved using OF<inline-formula><mml:math id="M6" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, overcoming the limitation of many state-of-the-art potential hydrodynamic codes that assume small displacements of the platform. In addition, all the necessary information for the FOWT calculation and design processes can be obtained simultaneously, such as the pressure distribution at the platform components and the loads at the tower base, fairleads tension, etc. Moreover, the effect of turbulent winds and/or elastic blades could be taken into account to resolve load cases from the design and certification standards.</p>
  </abstract>
    
<funding-group>
<award-group id="gs1">
<funding-source>Gobierno de Navarra</funding-source>
<award-id>0011-1383-2022-000000</award-id>
</award-group>
</funding-group>
</article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction</title>
      <p id="d1e193">Floating offshore wind turbine (FOWT) design and optimization are necessary to accomplish the requirements with regard to the increase in wind energy capacity installed worldwide. The reduction in the levelized cost of energy (LCOE) of offshore wind energy will be possible, among others, if the fidelity of the tools used to design an FOWT is improved without a great increase in computational time. In addition, the coupling of the wind turbine and platform dynamics is necessary to the ensemble optimizations required in wind turbine and platform co-design processes.</p>
      <p id="d1e196">Most of the state-of-the-art hydrodynamic models used in engineering simulation tools, for the coupled analysis of<?pagebreak page1598?> FOWTs, are based on two different hydrodynamic models to resolve the hydrodynamic loads on the floating platform: Morison's equation (ME) and potential flow (PF) theory. The ME (see <xref ref-type="bibr" rid="bib1.bibx21" id="altparen.1"/>) can be applied to slender bodies and provides the inertia and drag forces over these elements. The PF (see <xref ref-type="bibr" rid="bib1.bibx22 bib1.bibx9" id="altparen.2"/>) is applicable to general geometries to solve the hydrodynamic problem, thereby obtaining the added mass, radiation damping, diffraction forces, etc., but does not include viscous effects. The viscous effects can be added to potential models through the drag term of Morison's equation or by adjusting the damping of the platform based on experimental data (see <xref ref-type="bibr" rid="bib1.bibx1" id="altparen.3"/>) or computational fluid dynamics (CFD) simulations. This potential solution can be obtained both in the frequency and in the time domains. Moreover, the forces and moments obtained by solving the potential problem in the frequency domain can be introduced into a time domain solver of the floating platform; see for example <xref ref-type="bibr" rid="bib1.bibx13" id="text.4"/>.</p>
      <p id="d1e211">As mentioned before, the hydrodynamic response of floating platforms can also be modeled by performing high-fidelity CFD simulations. This method has nowadays become a part of the design process of FOWTs. These simulations support the design process and allow the tuning of the integrated numerical tools since the early stages of the process so that the effort put into  wave tank testing is not lost once a mature platform design has been achieved. CFD simulations are used to provide quantitative information about the design process such as the damping coefficients needed in the engineering codes. In addition, flow phenomena such as wave run-up or pressures over the structure, or the heave plates, are provided to optimize the platform design and to understand its dynamics. Several publications can be found in which CFD is applied to simulate platform hydrodynamics. For instance, the OC6 Phase I collaborative work under the IEA Task 30 provided two publications; in the first one the platform's response to bi-chromatic waves was analyzed in <xref ref-type="bibr" rid="bib1.bibx30" id="text.5"/>, placing special focus on the wave treatment, pressures over the structure and wave run-up analysis. In the second one, free decay simulations were performed to make a benchmark between different CFD codes, including a detailed comparison with experiments described in  <xref ref-type="bibr" rid="bib1.bibx31" id="text.6"/>. Both publications demonstrated the potential of CFD use in platform design and characterization and pointed out the differences with regard to potential flow solver simulations. For example, it has been found that the potential flow solution used in <xref ref-type="bibr" rid="bib1.bibx30" id="text.7"/> significantly underpredicts the damping of surge motion. Another study from <xref ref-type="bibr" rid="bib1.bibx32" id="text.8"/> delves deeper into the effect of irregular waves on the DeepCWind platform, lending credibility to and confidence in the use of high-fidelity CFD simulations in predicting the global performance of floating wind platforms and for tuning mid-fidelity engineering models.</p>
      <p id="d1e226">On the other hand, rotor aerodynamics are simulated in the wind energy industry with different fidelity level tools ranging from blade element momentum theory (BEMT) <xref ref-type="bibr" rid="bib1.bibx4 bib1.bibx3" id="paren.9"/>, more complex free vortex filament methods (FVMs) <xref ref-type="bibr" rid="bib1.bibx15 bib1.bibx18" id="paren.10"/>, actuator line approaches <xref ref-type="bibr" rid="bib1.bibx24 bib1.bibx5" id="paren.11"/> and high-fidelity fully resolved CFD simulations. Typically, BEMT and FVM approaches are used for coupled aeroelastic simulations, while the different CFD approaches are used in purely aerodynamic simulations without considering the coupling with flexible degrees of freedom. Moreover, CFD is mainly used on the airfoil level or in specific cases in which extreme aerodynamic events need to be deeply analyzed. Recently, in the OC6 Phase III project numerous aerodynamic models with different fidelity levels have been compared, in purely aerodynamic conditions, with wind tunnel experimental data of a wind turbine placed over a moving structure capable of imposing displacements and rotations on the tower base of the wind turbine <xref ref-type="bibr" rid="bib1.bibx2" id="paren.12"/>. This study has shown that all analyzed aerodynamic models are capable of accurately predicting the aerodynamic loads under the forced pitch and surge motion studied in this OC6 Phase III project. However, it has been found that when considering the additional dynamics introduced by the controller, the aerodynamic cycles change.</p>
      <p id="d1e242">Furthermore, the combined hydro-aero high-fidelity simulation of FOWTs under wind and wave conditions is a cutting-edge technology with few research works available in the literature <xref ref-type="bibr" rid="bib1.bibx23 bib1.bibx20" id="paren.13"/>. In addition, in the few existing models it is very rare to see couplings with elastic models of the flexible elements of the wind turbine, such as the blades or the tower. And it is even more difficult to find models that include the coupling with the wind turbine control system. <xref ref-type="bibr" rid="bib1.bibx25" id="text.14"/> conducted a CFD analysis of the NREL 5 MW with a TLP structure under wind and wave conditions and simulated it with the commercial software Fluent. In that work only the surge motion was allowed. In their work, <xref ref-type="bibr" rid="bib1.bibx17" id="text.15"/> presented  a coupled CFD simulation using OpenFOAM both in the rotor and in the floating platform. No information was provided about the computational time of their simulations. <xref ref-type="bibr" rid="bib1.bibx29" id="text.16"/> carried out fully coupled aerodynamic–hydrodynamic simulations of the OC4 DeepCWind semi-submersible with a wind turbine using CFD and a catenary mooring solver. The major FOWT components were simulated without considering structure deformations. The results considering free decay tests and regular wave conditions showed good agreement with the MARIN tests and the FAST code. <xref ref-type="bibr" rid="bib1.bibx34" id="text.17"/> also carried out fully coupled aerodynamic–hydrodynamic simulations of the DeepCwind semi-submersible with the NREL 5 MW wind turbine and also compared it with experimental measurements of the OC5 project <xref ref-type="bibr" rid="bib1.bibx28" id="paren.18"/>. In this work, the simulation time for one case was 20 d with 66 CPUs. In addition,<?pagebreak page1599?> it was found that the power output is more sensitive than the thrust force to platform motions.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><?xmltex \currentcnt{1}?><?xmltex \def\figurename{Figure}?><label>Figure 1</label><caption><p id="d1e266">Visualization of an OF<inline-formula><mml:math id="M7" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulation. The forces on the blades are shown alongside the mooring line tension and the dynamic pressure on the platform.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f01.png"/>

      </fig>

      <p id="d1e284">Moreover, in the design and certification process of FOWTs, following standards such as the IEC 61400-3-2 Ed1 <xref ref-type="bibr" rid="bib1.bibx11" id="paren.19"/> or NI572 <xref ref-type="bibr" rid="bib1.bibx6" id="paren.20"/>, the hydrodynamic pressure over the surface of the platform may be requested alongside the loads at the tower base or mooring tensions at the fairleads for different cases with the wind turbine in a normal operational state, storms or under fault conditions. Even more, some specific FOWT designs equipped with single-point mooring (SPM) may have large rotations in order to weather vane with the wind, which can violate some limitations or assumptions of the state-of-the-art design codes like OpenFAST (see <xref ref-type="bibr" rid="bib1.bibx14" id="altparen.21"/>). Therefore, a new simulation tool is presented in this work, called OF<inline-formula><mml:math id="M8" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, which combines a high-fidelity representation of the hydrodynamic behavior of the floating platform with an aero-servo-elastic representation of the tower and rotor nacelle assembly. This approach reduces the computational time with regard to full CFD simulations of FOWTs, allowing us to introduce the control system into the simulation and include flexible responses of the different FOWT components. The dynamic pressure, mooring tension, wave run-up and body forces can be obtained as in the visualization example that has been represented in Fig. <xref ref-type="fig" rid="Ch1.F1"/>.</p>
      <p id="d1e307">The rest of the article is organized as follows: the methodology used to couple OpenFAST and OpenFOAM is defined in Sect. <xref ref-type="sec" rid="Ch1.S2"/>, and then the verification methodology is included in Sect. <xref ref-type="sec" rid="Ch1.S3"/>. It includes, firstly, the description of the simulated load cases  to demonstrate the applicability of the method and the advantages with regard to potential codes or fully resolved CFD simulations. Secondly, the FOWT model used to test OF<inline-formula><mml:math id="M9" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> is described as well as the simulation setup and the results. Finally, the conclusions of this work are presented in Sect. <xref ref-type="sec" rid="Ch1.S4"/>.</p>
</sec>
<sec id="Ch1.S2">
  <label>2</label><?xmltex \opttitle{OF${}^{2}$ methodology: OpenFAST and OpenFOAM coupling}?><title>OF<inline-formula><mml:math id="M10" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> methodology: OpenFAST and OpenFOAM coupling</title>
      <p id="d1e343">In this work OpenFAST and OpenFOAM are coupled in order to better simulate the floating platform's hydrodynamic response and to overcome engineering model limitations. With the following approach, the aero-servo-elastic response of the wind turbine is simulated with OpenFAST, while the floating platform dynamics and fluid flow are simulated with OpenFOAM. The resulting tool has been named OF<inline-formula><mml:math id="M11" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2" specific-use="star"><?xmltex \currentcnt{2}?><?xmltex \def\figurename{Figure}?><label>Figure 2</label><caption><p id="d1e357">Flowchart of the OF<inline-formula><mml:math id="M12" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> coupling process.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f02.png"/>

      </fig>

      <p id="d1e375">Hence, this OF<inline-formula><mml:math id="M13" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> environment has been made through the development of  two new shared libraries. The operation scheme of all the OF<inline-formula><mml:math id="M14" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> libraries within OpenFOAM can be seen in Fig. <xref ref-type="fig" rid="Ch1.F2"/>. Firstly, <monospace>libForcedOpenFAST.so</monospace> has been developed. This library allows us to run OpenFAST, imposing the floating platform displacements (see <xref ref-type="bibr" rid="bib1.bibx19" id="altparen.22"/>, for the details of the imposition of movements in OpenFAST). Secondly, a new rigid-body-motion-type restraint, named <monospace>libOF2.so</monospace>, has also been created. This <monospace>libOF2.so</monospace> restraint uses the functions existing inside <monospace>libForcedOpenFAST.so</monospace> in order to apply the loads computed by OpenFAST on the rigid body, i.e., the floating platform. Therefore, at each time step, the floating platform dynamics is solved by the rigid body motion library within OpenFOAM. When the OF<inline-formula><mml:math id="M15" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> restraint is executed, it uses the displacement, velocity and acceleration of the floating platform as an input for the functions of <monospace>libForcedOpenFAST.so</monospace> that impose this displacement onto the wind turbine modeled within OpenFAST and that calculate the corresponding loads, power and deformations of the different wind turbine components. Finally, the loads at the tower base point are then applied to OpenFOAM's body, along with the ones resulting from the other restraints (like mooring lines or external forces if any) and fluid forces. Once the platform's dynamics response is solved, the mesh is updated and adapted to the new platform's position, and the fluid flow is solved finishing the current time step iteration. This approach ensures that the effect of the platform dynamics on the tower and rotor nacelle assembly is considered in  the servo, elastic and aerodynamic responses of each of these components and vice versa. An example of a simplified dynamicMeshDict file used in OpenFOAM to describe the body dynamics using the new shared libraries can be seen in Appendix <xref ref-type="sec" rid="App1.Ch1.S1"/>.</p>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>Verification of the methodology</title>
<sec id="Ch1.S3.SS1">
  <label>3.1</label><title>Load cases</title>
      <p id="d1e443">In order to verify OF<inline-formula><mml:math id="M16" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, two verification load cases have been evaluated with OF<inline-formula><mml:math id="M17" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> and an OpenFAST-only approach. The two cases have been based on load case (LC) 3.1 of the OC4 project <xref ref-type="bibr" rid="bib1.bibx27" id="paren.23"/>, with a steady uniform (deterministic) wind speed of <inline-formula><mml:math id="M18" display="inline"><mml:mn mathvariant="normal">8</mml:mn></mml:math></inline-formula> m s<inline-formula><mml:math id="M19" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, a regular wave height (<inline-formula><mml:math id="M20" display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula>) of <inline-formula><mml:math id="M21" display="inline"><mml:mn mathvariant="normal">6</mml:mn></mml:math></inline-formula> m and a period (<inline-formula><mml:math id="M22" display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula>) of <inline-formula><mml:math id="M23" display="inline"><mml:mn mathvariant="normal">10</mml:mn></mml:math></inline-formula> s. In the first load case analyzed in this work, called <inline-formula><mml:math id="M24" display="inline"><mml:mrow><mml:msup><mml:mn mathvariant="normal">3.1</mml:mn><mml:mo>*</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>, no waves have been included. All the main characteristics of these two load cases have been summarized in Table <xref ref-type="table" rid="Ch1.T1"/>.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T1" specific-use="star"><?xmltex \currentcnt{1}?><label>Table 1</label><caption><p id="d1e531">Description of the load cases analyzed, adapted from OC4 Phase II <xref ref-type="bibr" rid="bib1.bibx27" id="paren.24"/>.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="3">
     <oasis:colspec colnum="1" colname="col1" align="justify" colwidth="4cm"/>
     <oasis:colspec colnum="2" colname="col2" align="justify" colwidth="4cm"/>
     <oasis:colspec colnum="3" colname="col3" align="justify" colwidth="4cm"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Load case</oasis:entry>
         <oasis:entry colname="col2">3.1*</oasis:entry>
         <oasis:entry colname="col3">3.1</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Description</oasis:entry>
         <oasis:entry colname="col2">Deterministic at below rated</oasis:entry>
         <oasis:entry colname="col3">Deterministic at below rated</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Wind turbine initial condition</oasis:entry>
         <oasis:entry colname="col2"><inline-formula><mml:math id="M25" display="inline"><mml:mrow><mml:mi mathvariant="normal">Ω</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">9</mml:mn></mml:mrow></mml:math></inline-formula> rpm <?xmltex \hack{\hfill\break}?>blade pitch <inline-formula><mml:math id="M26" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <inline-formula><mml:math id="M27" display="inline"><mml:mn mathvariant="normal">0</mml:mn></mml:math></inline-formula><inline-formula><mml:math id="M28" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> <?xmltex \hack{\hfill\break}?>nacelle yaw <inline-formula><mml:math id="M29" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <inline-formula><mml:math id="M30" display="inline"><mml:mn mathvariant="normal">0</mml:mn></mml:math></inline-formula><inline-formula><mml:math id="M31" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3"><inline-formula><mml:math id="M32" display="inline"><mml:mrow><mml:mi mathvariant="normal">Ω</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">9</mml:mn></mml:mrow></mml:math></inline-formula> rpm <?xmltex \hack{\hfill\break}?>blade pitch <inline-formula><mml:math id="M33" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <inline-formula><mml:math id="M34" display="inline"><mml:mn mathvariant="normal">0</mml:mn></mml:math></inline-formula><inline-formula><mml:math id="M35" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> <?xmltex \hack{\hfill\break}?>nacelle yaw <inline-formula><mml:math id="M36" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <inline-formula><mml:math id="M37" display="inline"><mml:mn mathvariant="normal">0</mml:mn></mml:math></inline-formula><inline-formula><mml:math id="M38" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Enabled DOFs</oasis:entry>
         <oasis:entry colname="col2">All</oasis:entry>
         <oasis:entry colname="col3">All</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1">Wind condition</oasis:entry>
         <oasis:entry colname="col2">Steady, uniform, <?xmltex \hack{\hfill\break}?>no shear <?xmltex \hack{\hfill\break}?> <inline-formula><mml:math id="M39" display="inline"><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mi mathvariant="normal">hub</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M40" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <inline-formula><mml:math id="M41" display="inline"><mml:mn mathvariant="normal">8</mml:mn></mml:math></inline-formula> m s<inline-formula><mml:math id="M42" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3">Steady, uniform, <?xmltex \hack{\hfill\break}?>no shear <?xmltex \hack{\hfill\break}?> <inline-formula><mml:math id="M43" display="inline"><mml:mrow><mml:msub><mml:mi>V</mml:mi><mml:mi mathvariant="normal">hub</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M44" display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <inline-formula><mml:math id="M45" display="inline"><mml:mn mathvariant="normal">8</mml:mn></mml:math></inline-formula> m s<inline-formula><mml:math id="M46" display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula></oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Wave condition</oasis:entry>
         <oasis:entry colname="col2">No wave</oasis:entry>
         <oasis:entry colname="col3">Regular Stokes II: <?xmltex \hack{\hfill\break}?> <inline-formula><mml:math id="M47" display="inline"><mml:mrow><mml:mi>H</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula> m, <?xmltex \hack{\hfill\break}?> <inline-formula><mml:math id="M48" display="inline"><mml:mrow><mml:mi>T</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">10</mml:mn></mml:mrow></mml:math></inline-formula> s</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table><?xmltex \gdef\@currentlabel{1}?></table-wrap>

</sec>
<sec id="Ch1.S3.SS2">
  <label>3.2</label><title>Simulation setup</title>
      <p id="d1e862">The new tool, OF<inline-formula><mml:math id="M49" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, has been used to evaluate the response under wind and wave loading. For this study, OpenFAST v2.6.0 and OpenFOAM v21.06 have been coupled to model the NREL 5 MW wind turbine on the OC4 semi-submersible DeepCWind floating platform (see <xref ref-type="bibr" rid="bib1.bibx12" id="altparen.25"/>, and <xref ref-type="bibr" rid="bib1.bibx26" id="altparen.26"/>).</p>
      <p id="d1e880">The tower and rotor nacelle assemblies have been modeled considering the flexibility of the different components. For the three blades, two flexible modes in the flapwise direction and one in the edgewise direction have been considered. Additionally, for the drivetrain, a torsional mode has been included, and two flexible modes have also been <?pagebreak page1600?> considered, in both the fore–aft direction and the side–side direction, to represent the flexible response of the tower. The floating platform is considered to be a fully rigid structure. Furthermore, an in-house controller designed for this FOWT has been used.</p>
      <p id="d1e883">Moreover, the mooring system has been simulated using MoorDyn (see <xref ref-type="bibr" rid="bib1.bibx10" id="altparen.27"/>) and OpenFOAM's restraint developed by <xref ref-type="bibr" rid="bib1.bibx7" id="text.28"/>. This restraint has been modified to work together with  OpenFOAM's rigid body motion library, and it has been called <monospace>libmoordynRestraint.so</monospace>. The way to include this new restraint in the dynamicMeshDict is also included in Appendix <xref ref-type="sec" rid="App1.Ch1.S1"/>.</p>
      <p id="d1e897">For the CFD simulations performed inside OF<inline-formula><mml:math id="M50" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, an unstructured mesh has been created with snappyHexMesh, where the domain size is 581/403/278 m in the surge, sway and heave directions. The smaller element on the platform's surface mesh has a size of between 0.3 and 0.6 m, and no boundary layer has been added close to the body. Three refinement regions have been used: the first is a box around the floating platform where the mesh size is 0.6 m in the vertical direction with an aspect ratio of 4, and the other two are boxes located around the still-water level, ensuring a minimum of 20 cells per wave height and 50 cells per wave length, as suggested in <xref ref-type="bibr" rid="bib1.bibx8" id="text.29"/>. These settings result in 2.3 million element meshes. Different mesh details are shown in  Figs. <xref ref-type="fig" rid="Ch1.F3"/> (overall view), <xref ref-type="fig" rid="Ch1.F4"/> (platform body view) and <xref ref-type="fig" rid="Ch1.F5"/> (platform surrounding view).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3" specific-use="star"><?xmltex \currentcnt{3}?><?xmltex \def\figurename{Figure}?><label>Figure 3</label><caption><p id="d1e921">Overall view of the computational domain mesh.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f03.png"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><?xmltex \currentcnt{4}?><?xmltex \def\figurename{Figure}?><label>Figure 4</label><caption><p id="d1e932">Platform surface mesh.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f04.jpg"/>

        </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5" specific-use="star"><?xmltex \currentcnt{5}?><?xmltex \def\figurename{Figure}?><label>Figure 5</label><caption><p id="d1e943">Near-platform refinement.</p></caption>
          <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f05.png"/>

        </fig>

      <p id="d1e952">Regarding the numerical schemes used, first-order implicit laminar simulations with OpenFOAM v21.06 have been done. In particular, Gauss linear spatial schemes, for the gradient terms, and Gauss upwind and Gauss MUSCL<?pagebreak page1601?> schemes, for the divergence terms, have been used. Moreover, the MULES interface-capturing scheme has been selected. Finally, the PIMPLE algorithm has been used to solve the pressure–velocity coupling. The under-relaxation factors for both velocity and pressure have been set to 1. In order to take into account the displacements, a dynamic mesh approach is required to perform the simulation. Additionally, the displacement Laplacian, as the motion solver, and the moving wall, as the boundary condition in the floating platform, have been used. With an implicit algorithm the mesh morphing is updated at each iteration driven by the platform dynamics.  Finally, the  boundary conditions used are wave velocity inlet and pressure outlet in the inlet and outlet boundaries, the ground is considered a wall, and the domain sides are modeled with a slip condition. Moreover, the boundary condition used for wave generation uses a ramp timescale factor to avoid numerical divergence. In order to absorb the waves at the outlet, the shallowWaterAbsorption boundary condition has been used; this boundary condition applies a 0 gradient condition to the phase field and to the vertical component of the velocity, while it sets  the other two velocity components to 0. For the floating platform the movingWallVelocity boundary condition is used. The resulting wave elevation profile has an initial transitory state where the wave amplitude is gradually increased. This transient evolution is shown in Fig. <xref ref-type="fig" rid="Ch1.F6"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6"><?xmltex \currentcnt{6}?><?xmltex \def\figurename{Figure}?><label>Figure 6</label><caption><p id="d1e960">Wave elevation transient evolution.</p></caption>
          <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f06.png"/>

        </fig>

      <p id="d1e969">In order to analyze the OF<inline-formula><mml:math id="M51" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> performance, an OpenFAST-only model for comparison purposes has been created to define the integrated model of the FOWT. It has to be noted that the OpenFAST model for the tower and rotor nacelle assembly (RNA) is the same in the OpenFAST-only model and the coupled tool OF<inline-formula><mml:math id="M52" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>. In particular, the same blade element model (BEM) approach has been applied to compute the aerodynamic loads at the rotor, and the same wind files<?pagebreak page1602?> have been used in both simulations. The ElastoDyn representation of the tower and rotor nacelle assembly in OpenFAST is the same as that used in the OF<inline-formula><mml:math id="M53" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> solver. The same MoorDyn input files have been used for both simulations. It should be noted that the wave elevation signal used in the OpenFAST simulation of LC 3.1 has been extracted from an empty channel simulation performed with OpenFOAM, that is, from a simulation of the sea state without the floating platform. This wave elevation signal monitored at the platform's initial reference point (<inline-formula><mml:math id="M54" display="inline"><mml:mrow><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula> m) is used by OpenFAST to determine the loads that the waves exert onto the platform along the whole simulation. Therefore, the waves that affect the dynamics of both OpenFAST and OF<inline-formula><mml:math id="M55" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulations should be comparable, even though the actual wave in the OF<inline-formula><mml:math id="M56" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> approach is three-dimensional.</p>
      <?pagebreak page1603?><p id="d1e1030">In the OpenFAST-only simulations, the platform's hydrodynamic response has been represented through the HydroDyn module (see <xref ref-type="bibr" rid="bib1.bibx14" id="altparen.30"/>) with a combination of the potential flow and Morison equation. The drag coefficient of the members range between 0.56 and 0.68, depending on the diameter, as is defined in <xref ref-type="bibr" rid="bib1.bibx28" id="text.31"/>. A drag coefficient of 9.6 has been used for the heave plates, using the plate area as reference to compute the force. Non-linear hydrodynamics has been included using full quadratic transfer functions (QTFs). The LC 3.1<inline-formula><mml:math id="M57" display="inline"><mml:msup><mml:mi/><mml:mo>*</mml:mo></mml:msup></mml:math></inline-formula> case  has a simulation time of <inline-formula><mml:math id="M58" display="inline"><mml:mn mathvariant="normal">400</mml:mn></mml:math></inline-formula> s and LC 3.1 of <inline-formula><mml:math id="M59" display="inline"><mml:mn mathvariant="normal">1000</mml:mn></mml:math></inline-formula> s, both of them with a time step of <inline-formula><mml:math id="M60" display="inline"><mml:mn mathvariant="normal">0.01</mml:mn></mml:math></inline-formula> s. The OF<inline-formula><mml:math id="M61" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulations have been run on one node equipped with a dual AMD EPYC 7543 32-core processor and 128 GB of RAM.</p>
</sec>
<sec id="Ch1.S3.SS3">
  <label>3.3</label><title>Results</title>
      <p id="d1e1087">Hereafter, the results obtained by both approaches, OpenFAST only and OF<inline-formula><mml:math id="M62" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, are compared. Firstly, the time series results of the platform's degrees of freedom (DOFs) and loads are compared in order to have a qualitative comparison of the results obtained from both OF<inline-formula><mml:math id="M63" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> and OpenFAST-only approaches. Then, a quantitative comparison of the mean and standard deviation values of these DOFs is performed.</p>
<sec id="Ch1.S3.SS3.SSS1">
  <label>3.3.1</label><?xmltex \opttitle{Still-water case: LC~3.1${}^{*}$}?><title>Still-water case: LC 3.1<inline-formula><mml:math id="M64" display="inline"><mml:msup><mml:mi/><mml:mo>*</mml:mo></mml:msup></mml:math></inline-formula></title>
      <p id="d1e1124">The results corresponding to the still-water case, LC 3.1<inline-formula><mml:math id="M65" display="inline"><mml:msup><mml:mi/><mml:mo>*</mml:mo></mml:msup></mml:math></inline-formula>, can be seen in Fig. <xref ref-type="fig" rid="Ch1.F7"/>. This figure includes the results obtained for surge (top), heave (middle) and pitch (bottom) motions (left column) and the respective loads (right column).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7" specific-use="star"><?xmltex \currentcnt{7}?><?xmltex \def\figurename{Figure}?><label>Figure 7</label><caption><p id="d1e1140">Platform responses <bold>(a, c, e)</bold> and hydrodynamic loads <bold>(b, d, f)</bold> in surge <bold>(a, b)</bold>, heave <bold>(c, d)</bold> and pitch motions <bold>(e, f)</bold>, as well as degrees of freedom in the still-water case, LC 3.1<inline-formula><mml:math id="M66" display="inline"><mml:msup><mml:mi/><mml:mo>*</mml:mo></mml:msup></mml:math></inline-formula>. The results obtained with OpenFAST have been presented in blue, while those obtained with OF<inline-formula><mml:math id="M67" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> have been represented in orange.</p></caption>
            <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f07.png"/>

          </fig>

      <p id="d1e1183">As can be seen in Fig. <xref ref-type="fig" rid="Ch1.F7"/>a, c and e, OF<inline-formula><mml:math id="M68" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> is able to properly model the dynamic behavior of the FOWT. The surge motions for both of the compared approaches present similar values in terms of the period, mean value and amplitude. However, slight differences in the amplitude arise due to the different modeling of hydrodynamic loads. For the heave response, it must be noted that there is a difference of less than 0.1 m between the mean value of both simulations. It is considered that this offset of around 0.5 % of the platform's draft is caused by the difference in the submerged volume. In OF<inline-formula><mml:math id="M69" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> this volume is not user defined but is a result of the surface mesh employed – using a different refinement on the surface mesh would lead to a smaller heave offset, but this deviation can be assumed to be negligible. The comparison between the pitch responses demonstrates the OF<inline-formula><mml:math id="M70" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> feasibility, and, therefore, it can be assumed that the OF<inline-formula><mml:math id="M71" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> approach is verified.</p>
      <p id="d1e1225"><?xmltex \hack{\newpage}?>Figure <xref ref-type="fig" rid="Ch1.F7"/>b, d and f compare the resulting hydrodynamic loads acting on the platform for each modeling approach for the deterministic case without waves, LC 3.1<inline-formula><mml:math id="M72" display="inline"><mml:msup><mml:mi/><mml:mo>*</mml:mo></mml:msup></mml:math></inline-formula>. Note that moments are computed with regard to the platform reference point. In particular, the loads computed under the OF<inline-formula><mml:math id="M73" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> approach are those exerted by the fluid on the platform, i.e., both the hydrodynamic and the hydrostatic loads. The demanded load outputs under the OpenFAST approach are the integrated hydrodynamic loads, and they also take hydrostatic forces into account. Therefore, it must be noted that both approaches determine similar mean loads and that the surge force and pitch moment are very similar. The small-scale differences in the heave force amplitudes are caused by the larger motions of the OF<inline-formula><mml:math id="M74" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulation, which is initialized at a farther position from its equilibrium, compared to the OpenFAST-only simulation. A comparison of the disaggregated loads (hydrostatic and hydrodynamic) has also been  performed, showing the same trend.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8" specific-use="star"><?xmltex \currentcnt{8}?><?xmltex \def\figurename{Figure}?><label>Figure 8</label><caption><p id="d1e1260">Platform response <bold>(a, c, e)</bold> and hydrodynamic loads <bold>(b, d, f)</bold> in surge <bold>(a, b)</bold>, heave <bold>(c, d)</bold> and pitch motions <bold>(e, f)</bold>, as well as degrees of freedom in the regular wave case, LC 3.1. The results obtained with OpenFAST have been presented in blue, while those obtained with OF<inline-formula><mml:math id="M75" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> have been represented in orange.</p></caption>
            <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f08.png"/>

          </fig>

</sec>
<sec id="Ch1.S3.SS3.SSS2">
  <label>3.3.2</label><title>Regular wave case: LC 3.1</title>
      <p id="d1e1302">The regular wave case (LC 3.1) time series are presented in Fig. <xref ref-type="fig" rid="Ch1.F8"/>, following the same scheme as for the previous case, showing the platform's degrees of freedom in the left column and the hydrodynamic loads in the right column.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T2" specific-use="star"><?xmltex \currentcnt{2}?><label>Table 2</label><caption><p id="d1e1310">Statistical results of the different variables analyzed for the load case under wind and waves, LC 3.1. The standard deviation (SD) and the mean values (mean) for each model used, OpenFAST and OF<inline-formula><mml:math id="M76" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, have been included alongside the normalized differences obtained between the two models following Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>).</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="8">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="left"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:colspec colnum="4" colname="col4" align="right" colsep="1"/>
     <oasis:colspec colnum="5" colname="col5" align="right"/>
     <oasis:colspec colnum="6" colname="col6" align="right" colsep="1"/>
     <oasis:colspec colnum="7" colname="col7" align="right"/>
     <oasis:colspec colnum="8" colname="col8" align="right"/>
     <oasis:thead>
       <oasis:row>
         <oasis:entry colname="col1">Variable</oasis:entry>
         <oasis:entry colname="col2">Units</oasis:entry>
         <oasis:entry rowsep="1" namest="col3" nameend="col4" align="center" colsep="1">OpenFAST </oasis:entry>
         <oasis:entry rowsep="1" namest="col5" nameend="col6" align="center" colsep="1">OF<inline-formula><mml:math id="M77" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula></oasis:entry>
         <oasis:entry rowsep="1" namest="col7" nameend="col8" align="center">Diff [%] </oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2"/>
         <oasis:entry colname="col3">SD</oasis:entry>
         <oasis:entry colname="col4">mean</oasis:entry>
         <oasis:entry colname="col5">SD</oasis:entry>
         <oasis:entry colname="col6">mean</oasis:entry>
         <oasis:entry colname="col7">SD</oasis:entry>
         <oasis:entry colname="col8">mean</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">Platform surge</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">3.36</oasis:entry>
         <oasis:entry colname="col4">4.72</oasis:entry>
         <oasis:entry colname="col5">5.86</oasis:entry>
         <oasis:entry colname="col6">7.7</oasis:entry>
         <oasis:entry colname="col7">74.54</oasis:entry>
         <oasis:entry colname="col8">63.19</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Platform sway</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">0.01</oasis:entry>
         <oasis:entry colname="col4">0.00</oasis:entry>
         <oasis:entry colname="col5">2.37</oasis:entry>
         <oasis:entry colname="col6">0.01</oasis:entry>
         <oasis:entry colname="col7">29 178</oasis:entry>
         <oasis:entry colname="col8">176.58</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Platform heave</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">0.55</oasis:entry>
         <oasis:entry colname="col4">0.05</oasis:entry>
         <oasis:entry colname="col5">0.11</oasis:entry>
         <oasis:entry colname="col6"><inline-formula><mml:math id="M78" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.05</oasis:entry>
         <oasis:entry colname="col7"><inline-formula><mml:math id="M79" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>7.63</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M80" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>198.42</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Platform roll</oasis:entry>
         <oasis:entry colname="col2">(deg)</oasis:entry>
         <oasis:entry colname="col3">0.02</oasis:entry>
         <oasis:entry colname="col4">0.10</oasis:entry>
         <oasis:entry colname="col5">0.16</oasis:entry>
         <oasis:entry colname="col6">0.10</oasis:entry>
         <oasis:entry colname="col7"><inline-formula><mml:math id="M81" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>951.02</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M82" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.04</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Platform pitch</oasis:entry>
         <oasis:entry colname="col2">(deg)</oasis:entry>
         <oasis:entry colname="col3">0.93</oasis:entry>
         <oasis:entry colname="col4">1.86</oasis:entry>
         <oasis:entry colname="col5">0.91</oasis:entry>
         <oasis:entry colname="col6">1.74</oasis:entry>
         <oasis:entry colname="col7"><inline-formula><mml:math id="M83" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.6</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M84" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>6.45</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Platform yaw</oasis:entry>
         <oasis:entry colname="col2">(deg)</oasis:entry>
         <oasis:entry colname="col3">0.03</oasis:entry>
         <oasis:entry colname="col4"><inline-formula><mml:math id="M85" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.06</oasis:entry>
         <oasis:entry colname="col5">2.41</oasis:entry>
         <oasis:entry colname="col6"><inline-formula><mml:math id="M86" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.08</oasis:entry>
         <oasis:entry colname="col7">7444.84</oasis:entry>
         <oasis:entry colname="col8">36.78</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Blade tip in-plane displacement</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">0.33</oasis:entry>
         <oasis:entry colname="col4"><inline-formula><mml:math id="M87" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.30</oasis:entry>
         <oasis:entry colname="col5">0.33</oasis:entry>
         <oasis:entry colname="col6"><inline-formula><mml:math id="M88" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.30</oasis:entry>
         <oasis:entry colname="col7">0.42</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M89" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.91</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Blade tip out-of-plane displacement</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">0.29</oasis:entry>
         <oasis:entry colname="col4">3.23</oasis:entry>
         <oasis:entry colname="col5">0.30</oasis:entry>
         <oasis:entry colname="col6">3.20</oasis:entry>
         <oasis:entry colname="col7">3.47</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M90" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.91</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Tower top fore–aft displacement</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">0.07</oasis:entry>
         <oasis:entry colname="col4">0.21</oasis:entry>
         <oasis:entry colname="col5">0.07</oasis:entry>
         <oasis:entry colname="col6">0.20</oasis:entry>
         <oasis:entry colname="col7"><inline-formula><mml:math id="M91" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.28</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M92" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>2.57</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Tower top side–side displacement</oasis:entry>
         <oasis:entry colname="col2">(m)</oasis:entry>
         <oasis:entry colname="col3">0.01</oasis:entry>
         <oasis:entry colname="col4"><inline-formula><mml:math id="M93" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.02</oasis:entry>
         <oasis:entry colname="col5">0.01</oasis:entry>
         <oasis:entry colname="col6"><inline-formula><mml:math id="M94" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.02</oasis:entry>
         <oasis:entry colname="col7">60.81</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M95" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.24</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Generator power</oasis:entry>
         <oasis:entry colname="col2">(kW)</oasis:entry>
         <oasis:entry colname="col3">107.88</oasis:entry>
         <oasis:entry colname="col4">1647.98</oasis:entry>
         <oasis:entry colname="col5">116.113</oasis:entry>
         <oasis:entry colname="col6">1624.99</oasis:entry>
         <oasis:entry colname="col7">7.6325</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M96" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.40</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Rotational speed</oasis:entry>
         <oasis:entry colname="col2">(rpm)</oasis:entry>
         <oasis:entry colname="col3">0.17</oasis:entry>
         <oasis:entry colname="col4">8.99</oasis:entry>
         <oasis:entry colname="col5">0.17</oasis:entry>
         <oasis:entry colname="col6">8.95</oasis:entry>
         <oasis:entry colname="col7"><inline-formula><mml:math id="M97" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>2.99</oasis:entry>
         <oasis:entry colname="col8"><inline-formula><mml:math id="M98" display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.44</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table><?xmltex \gdef\@currentlabel{2}?></table-wrap>

      <p id="d1e1868">When the wave excitation is considered (LC 3.1) on platform motions (Fig. <xref ref-type="fig" rid="Ch1.F8"/>a, c and e), differences arise mainly at the signal amplitude. The surge motion, which is mainly driven by wind load, has a different initial transient behavior. This is due to the initialization of the OpenFAST-only approach. Once both of the approaches are close to the stationary state the surge behavior becomes similar. Fig. <xref ref-type="fig" rid="Ch1.F8"/>c shows a different mean heave value. This responds to the same offset that has previously been seen in the LC 3.1<inline-formula><mml:math id="M99" display="inline"><mml:msup><mml:mi/><mml:mo>*</mml:mo></mml:msup></mml:math></inline-formula> case. However, the pitch motion in OF<inline-formula><mml:math id="M100" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> shows an amplitude modulation that is not appreciated in the previous degrees of freedom (Fig. <xref ref-type="fig" rid="Ch1.F8"/>a and c), while it presents a similar mean value to the OpenFAST result. If the loads are analyzed (Fig. <xref ref-type="fig" rid="Ch1.F8"/>b, d and f), this modulation is also observed in the pitching moment. This is caused by how the wave evolves in OF<inline-formula><mml:math id="M101" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>. In order to show this effect, the wave elevation time series from both the empty channel (represented in blue and used in OpenFAST) and the OF<inline-formula><mml:math id="M102" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulation (represented in orange and measured 50 m upstream of the platform) have been included in Fig. <xref ref-type="fig" rid="Ch1.F9"/>. In Fig. <xref ref-type="fig" rid="Ch1.F9"/> an amplitude modulation is also observed on the OF<inline-formula><mml:math id="M103" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> wave elevation signal, which leads to the unexpected behaviors mentioned previously. Before running the OF<inline-formula><mml:math id="M104" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulation, the wave generation and numerical schemes were calibrated at the origin position in an empty numerical wave tank. The free surface elevation was not sampled in any other location. Due to the amplitude modulation, the wave generation test was performed again, and the same modulation 50 m upstream of the platform was seen. Numerical wave-makers have many sources of uncertainties and are the subject of many studies, as shown in <xref ref-type="bibr" rid="bib1.bibx33" id="text.32"/>. In the present work, static boundary methods have been used for both wave generation and absorption. In their research, <xref ref-type="bibr" rid="bib1.bibx33" id="text.33"/> found that static boundary methods were outperformed by relaxation zone methods. This may be due to the assumption of shallow-water conditions for wave absorption. Wave modulation is related to the wave generation method employed, and it should be improved in order to obtain the desired regular wave. Furthermore, these inconsistencies in the wave elevation mean that this OF<inline-formula><mml:math id="M105" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> result is not directly comparable with the results of <xref ref-type="bibr" rid="bib1.bibx26" id="text.34"/> in terms, for example, of the phase shift between the wave and the hydrodynamic forces in heave or pitch. Moreover, floating offshore wind turbines demand a long time of simulation, which has been found <xref ref-type="bibr" rid="bib1.bibx16" id="paren.35"/> to require suitable numerical schemes in order to keep the wave shape during the whole simulation. Considering all the aforementioned factors, it is asserted that wave generation and absorption hold utmost significance in FOWT simulations.<?pagebreak page1605?> Accordingly, a thorough calibration of the numerical wave tank should always be performed.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9"><?xmltex \currentcnt{9}?><?xmltex \def\figurename{Figure}?><label>Figure 9</label><caption><p id="d1e1963">Comparison between wave elevation signals. The OF<inline-formula><mml:math id="M106" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> signal is measured at <inline-formula><mml:math id="M107" display="inline"><mml:mrow><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mn mathvariant="normal">50</mml:mn></mml:mrow></mml:math></inline-formula> m</p></caption>
            <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f09.png"/>

          </fig>

      <p id="d1e1995">Nevertheless, since the OF<inline-formula><mml:math id="M108" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> approach solves the fluid domain, the pressure distribution on the platform surface, among other outputs, is available for further analysis, reinforcing the suitability of this tool for co-design processes, and also to support certification processes. For example, in Fig. <xref ref-type="fig" rid="Ch1.F10"/>, the dynamic pressure distribution over the floating platform is shown at a particular instant of the simulation. In addition to the high-fidelity simulation of the platform dynamics, with OF<inline-formula><mml:math id="M109" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> it is also possible to include the control and flexibility response of the wind turbine with a lower computational effort than with a fully flexible CFD approach. Therefore, the flexible response predicted by OF<inline-formula><mml:math id="M110" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> at the tower top and the blade tip locations have been compared against OpenFAST-only simulations in Figs. <xref ref-type="fig" rid="Ch1.F11"/> and <xref ref-type="fig" rid="Ch1.F12"/>, respectively, only for LC 3.1 with regular wave. The comparison of these variables for the still-water case is not included<?pagebreak page1606?> for the sake of simplicity. In these figures it can be seen that the differences in amplitude, especially for the pitch platform rotation that has previously  been observed in Fig. <xref ref-type="fig" rid="Ch1.F8"/>e, are also visible in the tower top fore–aft displacement and blade tip out-of-plane deflection in Figs. <xref ref-type="fig" rid="Ch1.F11"/>a and <xref ref-type="fig" rid="Ch1.F12"/>a, respectively.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F10" specific-use="star"><?xmltex \currentcnt{10}?><?xmltex \def\figurename{Figure}?><label>Figure 10</label><caption><p id="d1e2040">LC 3.1 pressure distribution over the floating platform at a time of 300 s.</p></caption>
            <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f10.png"/>

          </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F11" specific-use="star"><?xmltex \currentcnt{11}?><?xmltex \def\figurename{Figure}?><label>Figure 11</label><caption><p id="d1e2051">Tower top deformations for the regular wave case, LC 3.1. Tower top fore–aft deflection <bold>(a)</bold> and tower top side–side deflection <bold>(b)</bold>. The results obtained with OpenFAST have been presented in blue, while those obtained with OF<inline-formula><mml:math id="M111" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> have been represented in orange.</p></caption>
            <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f11.png"/>

          </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F12" specific-use="star"><?xmltex \currentcnt{12}?><?xmltex \def\figurename{Figure}?><label>Figure 12</label><caption><p id="d1e2078">Blade tip deformations for the regular wave case, LC 3.1. Blade tip out-of-plane deflection <bold>(a)</bold> and blade tip in-plane deflection <bold>(b)</bold>. The results obtained with OpenFAST have been presented in blue, while those obtained with OF<inline-formula><mml:math id="M112" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> have been represented in orange.</p></caption>
            <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f12.png"/>

          </fig>

      <p id="d1e2102">Moreover, the control performance for the regular wave case LC 3.1 is presented in Fig. <xref ref-type="fig" rid="Ch1.F13"/>. Both rotational speed (Fig. <xref ref-type="fig" rid="Ch1.F13"/>a) and generator power (Fig. <xref ref-type="fig" rid="Ch1.F13"/>b) present a slightly lower mean value and a smaller amplitude in OF<inline-formula><mml:math id="M113" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> than in the OpenFAST-only approach. These deviations are due to the differences in the FOWT movements.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F13" specific-use="star"><?xmltex \currentcnt{13}?><?xmltex \def\figurename{Figure}?><label>Figure 13</label><caption><p id="d1e2122">General regulation variables for the regular wave case, LC 3.1. The rotational speed <bold>(a)</bold> and the generator power <bold>(b)</bold>. The results obtained with OpenFAST have been presented in blue, while those obtained with OF<inline-formula><mml:math id="M114" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> have been represented in orange.</p></caption>
            <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-f13.png"/>

          </fig>

      <p id="d1e2146">Finally, the statistical analysis of all these time signals has been included in Table <xref ref-type="table" rid="Ch1.T2"/>. In this table, the standard deviation (SD) and the mean values (mean) for the two approaches compared in this work have been included. Additionally, the differences obtained between the two models have been quantified in terms of normal differences as shown in Eq. <xref ref-type="disp-formula" rid="Ch1.E1"/>:
              <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M115" display="block"><mml:mrow><mml:mi mathvariant="normal">Diff</mml:mi><mml:mo>[</mml:mo><mml:mi mathvariant="italic">%</mml:mi><mml:mo>]</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">100</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msup><mml:mi mathvariant="normal">OF</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>-</mml:mo><mml:mi mathvariant="normal">OpenFAST</mml:mi></mml:mrow><mml:mi mathvariant="normal">OpenFAST</mml:mi></mml:mfrac></mml:mstyle><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>
            Therefore, with this metric, if the difference is a positive value, it means the value in OF<inline-formula><mml:math id="M116" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> is higher than in the OpenFAST-only results. This metric has been applied for both the standard deviation and the mean value. It can be noted in Table <xref ref-type="table" rid="Ch1.T2"/> that the higher differences between OF<inline-formula><mml:math id="M117" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> and OpenFAST-only approaches are obtained in platform sway and heave DOFs. However, as these degrees of freedom have a very small range, it must be stated that the actual difference (without normalizing) is less than 10 mm in sway and 10 cm in heave. Although there have been shortcomings in wave generation, which can be further improved by employing alternative techniques, the presented metrics unequivocally establish the validity of the novel OF<inline-formula><mml:math id="M118" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> tool for the assessment of floating offshore wind turbines.</p>
      <?pagebreak page1607?><p id="d1e2217">The approach proposed in this work, using OF<inline-formula><mml:math id="M119" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> to perform coupled simulations of floating offshore wind turbines, presents advantages both over the lower-complexity resolution and over other high-fidelity approaches found in the literature. For example, when comparing OF<inline-formula><mml:math id="M120" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> capabilities with potential flow hydrodynamic solvers, OF<inline-formula><mml:math id="M121" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> allows us to include higher-order terms and viscous effects that are more difficult to fit in lower-complexity models like HydroDyn. Moreover, OF<inline-formula><mml:math id="M122" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> will allow us to overcome the limitation of HydroDyn that assumes small rotations for the platform response, thereby applying the hydrodynamic loads without updating these rotations and taking into account the actual position of the free surface. This advantage makes OF<inline-formula><mml:math id="M123" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> a recommendable tool for detailed analysis of the response of concepts equipped with SPM since they do not have any restrictions for rotation around the vertical axis. Additionally, OF<inline-formula><mml:math id="M124" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> presents lower computational costs than other fully coupled high-fidelity simulations found in the literature. Table <xref ref-type="table" rid="Ch1.T3"/> has been included to quantify this difference in computational cost. This table specifies the following  for each tool used in this study and for those from <xref ref-type="bibr" rid="bib1.bibx29" id="text.36"/> and <xref ref-type="bibr" rid="bib1.bibx34" id="text.37"/>: some details of the modeling methodology, the number of cores used for the simulation, the simulated time and the time it took to complete the simulation. As can be seen, OF<inline-formula><mml:math id="M125" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> has a much higher computational cost than the OpenFAST-only approach. However, it still allows 10 min load simulations to be carried out in less than 1 d. Moreover, with OF<inline-formula><mml:math id="M126" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, detailed simulations of complex cases can be addressed using less than 6 % of the computational resources necessary for a complete CFD approach for both aero- and hydrodynamics. Nevertheless, the computational cost in any CFD study depends mainly on the refinement of the mesh and the influence, for example, of certain calculation options. For instance, the meshes used in this study with OF<inline-formula><mml:math id="M127" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> do not have prismatic boundary layers, so the computational cost might not be fully comparable with those used in <xref ref-type="bibr" rid="bib1.bibx29" id="text.38"/> or <xref ref-type="bibr" rid="bib1.bibx34" id="text.39"/>.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T3" specific-use="star"><?xmltex \currentcnt{3}?><label>Table 3</label><caption><p id="d1e2321">Computational cost of different tools used for the coupled analysis of FOWT under wind and wave loading.</p></caption><oasis:table frame="topbot"><?xmltex \begin{scaleboxenv}{.90}[.90]?><oasis:tgroup cols="9">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="left"/>
     <oasis:colspec colnum="3" colname="col3" align="left"/>
     <oasis:colspec colnum="4" colname="col4" align="left"/>
     <oasis:colspec colnum="5" colname="col5" align="left"/>
     <oasis:colspec colnum="6" colname="col6" align="left"/>
     <oasis:colspec colnum="7" colname="col7" align="right"/>
     <oasis:colspec colnum="8" colname="col8" align="left"/>
     <oasis:colspec colnum="9" colname="col9" align="right"/>
     <oasis:thead>
       <oasis:row>
         <oasis:entry colname="col1">Tool</oasis:entry>
         <oasis:entry colname="col2">Hydrodynamic</oasis:entry>
         <oasis:entry colname="col3">Aerodynamic</oasis:entry>
         <oasis:entry colname="col4">Flexibility</oasis:entry>
         <oasis:entry colname="col5">Controller</oasis:entry>
         <oasis:entry colname="col6">Simulated</oasis:entry>
         <oasis:entry colname="col7">Cores</oasis:entry>
         <oasis:entry colname="col8">Wall-clock</oasis:entry>
         <oasis:entry colname="col9">Core hours</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2"/>
         <oasis:entry colname="col3"/>
         <oasis:entry colname="col4"/>
         <oasis:entry colname="col5"/>
         <oasis:entry colname="col6">time</oasis:entry>
         <oasis:entry colname="col7"/>
         <oasis:entry colname="col8">time</oasis:entry>
         <oasis:entry colname="col9"/>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">OpenFAST</oasis:entry>
         <oasis:entry colname="col2">PF and ME</oasis:entry>
         <oasis:entry colname="col3">BEMT</oasis:entry>
         <oasis:entry colname="col4">Yes</oasis:entry>
         <oasis:entry colname="col5">Yes</oasis:entry>
         <oasis:entry colname="col6">1000 s</oasis:entry>
         <oasis:entry colname="col7">1</oasis:entry>
         <oasis:entry colname="col8">7 min</oasis:entry>
         <oasis:entry colname="col9">0.1167</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">OF<inline-formula><mml:math id="M128" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">CFD-URANS</oasis:entry>
         <oasis:entry colname="col3">BEMT</oasis:entry>
         <oasis:entry colname="col4">Yes</oasis:entry>
         <oasis:entry colname="col5">Yes</oasis:entry>
         <oasis:entry colname="col6">1000 s</oasis:entry>
         <oasis:entry colname="col7">64</oasis:entry>
         <oasis:entry colname="col8">33.5 h</oasis:entry>
         <oasis:entry colname="col9">2142</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><xref ref-type="bibr" rid="bib1.bibx29" id="text.40"/></oasis:entry>
         <oasis:entry colname="col2">CFD-URANS</oasis:entry>
         <oasis:entry colname="col3">CFD-URANS</oasis:entry>
         <oasis:entry colname="col4">No</oasis:entry>
         <oasis:entry colname="col5">No</oasis:entry>
         <oasis:entry colname="col6">500 s</oasis:entry>
         <oasis:entry colname="col7">32</oasis:entry>
         <oasis:entry colname="col8">24 d</oasis:entry>
         <oasis:entry colname="col9">18 432</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><xref ref-type="bibr" rid="bib1.bibx34" id="text.41"/></oasis:entry>
         <oasis:entry colname="col2">CFD-URANS</oasis:entry>
         <oasis:entry colname="col3">CFD-URANS</oasis:entry>
         <oasis:entry colname="col4">No</oasis:entry>
         <oasis:entry colname="col5">No</oasis:entry>
         <oasis:entry colname="col6">300 s</oasis:entry>
         <oasis:entry colname="col7">66</oasis:entry>
         <oasis:entry colname="col8">20 d</oasis:entry>
         <oasis:entry colname="col9">31 680</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup><?xmltex \end{scaleboxenv}?></oasis:table><?xmltex \gdef\@currentlabel{3}?></table-wrap>

</sec>
</sec>
</sec>
<sec id="Ch1.S4" sec-type="conclusions">
  <label>4</label><title>Conclusions</title>
      <p id="d1e2554">A new simulation tool, called OF<inline-formula><mml:math id="M129" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, for time domain simulations of FOWT has been developed. The main conclusions of this work can be summarized as follows:</p>
      <p id="d1e2566"><list list-type="bullet">
          <list-item>

      <p id="d1e2571">OF<inline-formula><mml:math id="M130" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> combines a high-fidelity resolution of the hydrodynamic response of a floating platform with a multi-complexity aero-servo-elastic tool for the simulation of the wind turbine.</p>
          </list-item>
          <list-item>

      <p id="d1e2586">With the coupling of OpenFAST to a CFD simulation of the platform hydrodynamics, all the potential from OpenFAST can be used to introduce the wind turbine<?pagebreak page1608?> component flexible behavior, the turbulent winds and the control laws necessary for the FOWT operation.</p>
          </list-item>
          <list-item>

      <p id="d1e2592">The new tool has the advantage of reducing the computational time with regard to the use of a full CFD approach that includes the turbine aerodynamics.</p>
          </list-item>
          <list-item>

      <p id="d1e2598">Load cases with large platform displacements and wind turbine operation events can be simulated with OF<inline-formula><mml:math id="M131" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>. Current engineering tools present limitations in accurately capturing the effect of large displacements, and state-of-the-art CFD simulations typically consider rigid rotors.</p>
          </list-item>
          <list-item>

      <p id="d1e2613">OF<inline-formula><mml:math id="M132" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> has been verified in this study against OpenFAST-only simulations. The OC4 semi-submersible floating platform <xref ref-type="bibr" rid="bib1.bibx26" id="paren.42"/> and the NREL 5 MW wind turbine <xref ref-type="bibr" rid="bib1.bibx12" id="paren.43"/>, under co-directional wind and wave loading, have been used in this verification. The results have shown that the principal platform's degrees of freedom present very similar mean values between the OF<inline-formula><mml:math id="M133" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> and the OpenFAST-only approaches, in particular for the wind-only cases. Once the regular waves are introduced, higher differences arise, especially for the heave and pitch motions. It is likely that these differences are caused by a undesired loose of the wave amplitude in the OF<inline-formula><mml:math id="M134" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulation. Further research in  wave modeling should be done to improve the OF<inline-formula><mml:math id="M135" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> results.</p>
          </list-item>
          <list-item>

      <p id="d1e2663">In addition, as OF<inline-formula><mml:math id="M136" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> solves the complete fluid domain, it provides a detailed representation of the distributed magnitudes on the platform surface, which can be useful for the calculation and design process. For example, the pressure distribution at the platform components and the loads from the tower, the anchoring system, etc., can be obtained simultaneously.</p>
          </list-item>
          <list-item>

      <p id="d1e2678">OF<inline-formula><mml:math id="M137" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> could be used as part of the FOWT co-design techniques to optimize the design and, therefore, contribute to the reduction in LCOE of offshore wind energy.</p>
          </list-item>
          <list-item>

      <?pagebreak page1609?><p id="d1e2693">With OF<inline-formula><mml:math id="M138" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula>, an advance in the state of the art of simulation codes for FOWTs has been done. This will support the offshore wind energy cost reduction needed to boost the maturity of floating offshore wind energy.</p>
          </list-item>
        </list></p>
      <p id="d1e2707">In future work, OF<inline-formula><mml:math id="M139" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> will be used to analyze SPM designs to study weather-vaning responses under co-directional and misaligned wind and wave loading. Moreover, OF<inline-formula><mml:math id="M140" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> will be used to obtain the required distributed loads over the platform surface, along with the loads from the fairleads and tower base, to be used in a structural simulation tool for the analysis of ultimate and fatigue loads over the floating structure. OF<inline-formula><mml:math id="M141" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> will also be coupled with MUST <xref ref-type="bibr" rid="bib1.bibx19" id="paren.44"/>, an in-house tool based on OpenFAST, for the coupled analysis of multiple wind turbine floating platforms. This will allow analyzing the response of these types of configurations when equipped with SPM. MUST includes a free vortex filament method (FVM) module for the rotor aerodynamics, which will provide more accurate predictions of aerodynamic loads under the misaligned conditions that arise in large displacements of the system.</p><?xmltex \hack{\newpage}?>
</sec>

      
      </body>
    <back><app-group>

<app id="App1.Ch1.S1">
  <?xmltex \currentcnt{A}?><label>Appendix A</label><title>Extract of the dynamicMeshDict file</title><?xmltex \setfigures?><?xmltex \setlistings?><?xmltex \floatpos{h!}?><fig id="App1.Ch1.S1.F14"><?xmltex \currentcnt{A1}?><?xmltex \def\figurename{Listing}?><label>Listing A1</label><caption><p id="d1e2756">Configuration template for the OF<inline-formula><mml:math id="M142" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> and MoorDyn restraints in the dynamicMeshDict file.</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://wes.copernicus.org/articles/8/1597/2023/wes-8-1597-2023-l01.png"/>

      </fig>

<?xmltex \hack{\clearpage}?>
</app>
  </app-group><notes notes-type="dataavailability"><title>Data availability</title>

      <p id="d1e2780">Data will not be available a priori. If the data are needed for research or comparison purposes, the authors will be glad to share them upon request.</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d1e2786">GCA: tool development, methodology definition, verification, OF<inline-formula><mml:math id="M143" display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> simulations and writing. RMSR: tool development, verification, methodology definition, OpenFAST simulations and writing. PBC: tool development, methodology definition and verification. BML: funding acquisition, conceptual definition and writing. JAA: results analysis, verification and writing.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d1e2801">The contact author has declared that none of the authors has any competing interests.</p>
  </notes><notes notes-type="disclaimer"><title>Disclaimer</title>

      <p id="d1e2807">Publisher’s note: Copernicus Publications remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.</p>
  </notes><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d1e2813">This research has been supported by the Gobierno de Navarra (grant no. 0011-1383-2022-000000).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d1e2819">This paper was edited by Erin Bachynski-Polić and reviewed by two anonymous referees.</p>
  </notes><ref-list>
    <title>References</title>

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