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  <front>
    <journal-meta><journal-id journal-id-type="publisher">AMT</journal-id><journal-title-group>
    <journal-title>Atmospheric Measurement Techniques</journal-title>
    <abbrev-journal-title abbrev-type="publisher">AMT</abbrev-journal-title><abbrev-journal-title abbrev-type="nlm-ta">Atmos. Meas. Tech.</abbrev-journal-title>
  </journal-title-group><issn pub-type="epub">1867-8548</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/amt-14-2095-2021</article-id><title-group><article-title>LiSBOA (LiDAR Statistical Barnes Objective Analysis) for optimal design of lidar scans and retrieval of wind statistics – Part 2: Applications to lidar measurements of wind turbine wakes</article-title><alt-title>LiSBOA (LiDAR Statistical Barnes Objective Analysis) – Part 2</alt-title>
      </title-group><?xmltex \runningtitle{LiSBOA (LiDAR Statistical Barnes Objective Analysis) -- Part 2}?><?xmltex \runningauthor{S. Letizia et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="no">
          <name><surname>Letizia</surname><given-names>Stefano</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-5999-0131</ext-link></contrib>
        <contrib contrib-type="author" corresp="no">
          <name><surname>Zhan</surname><given-names>Lu</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="yes">
          <name><surname>Iungo</surname><given-names>Giacomo Valerio</given-names></name>
          <email>valerio.iungo@utdallas.edu</email>
        <ext-link>https://orcid.org/0000-0002-0990-8133</ext-link></contrib>
        <aff id="aff1"><institution>Wind Fluids and Experiments (WindFluX) Laboratory, Mechanical Engineering Department, The University of Texas at Dallas, 800 W Campbell Road, Richardson, TX 75080, USA</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Giacomo Valerio Iungo (valerio.iungo@utdallas.edu)</corresp></author-notes><pub-date><day>16</day><month>March</month><year>2021</year></pub-date>
      
      <volume>14</volume>
      <issue>3</issue>
      <fpage>2095</fpage><lpage>2113</lpage>
      <history>
        <date date-type="received"><day>11</day><month>June</month><year>2020</year></date>
           <date date-type="accepted"><day>22</day><month>January</month><year>2021</year></date>
           <date date-type="rev-recd"><day>20</day><month>January</month><year>2021</year></date>
           <date date-type="rev-request"><day>31</day><month>August</month><year>2020</year></date>
      </history>
      <permissions>
        <copyright-statement>Copyright: © 2021 Stefano Letizia et al.</copyright-statement>
        <copyright-year>2021</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://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021.html">This article is available from https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021.html</self-uri><self-uri xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021.pdf">The full text article is available as a PDF file from https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021.pdf</self-uri>
      <abstract><title>Abstract</title>
    <p id="d1e96">The LiDAR Statistical Barnes Objective Analysis (LiSBOA), presented in <xref ref-type="bibr" rid="bib1.bibx42" id="text.1"/>, is a procedure for the optimal design of lidar scans and calculations over a Cartesian grid of the statistical moments of the velocity field. Lidar data collected during a field campaign conducted at a wind farm in complex terrain are analyzed through LiSBOA for two different tests. For both case studies, LiSBOA is leveraged for the optimization of the azimuthal step of the lidar and the retrieval of the mean equivalent velocity and turbulence intensity fields. In the first case, the wake velocity statistics of four utility-scale turbines are reconstructed on a 3D grid, showing LiSBOA's ability to capture complex flow features, such as high-speed jets around the nacelle and the wake turbulent-shear layers. For the second case, the statistics of the wakes generated by four interacting turbines are calculated over a 2D Cartesian grid and compared to the measurements provided by the nacelle-mounted anemometers. Maximum discrepancies, as low as 3 % for the mean velocity (with respect to the free stream velocity) and turbulence intensity (in absolute terms), endorse the application of LiSBOA for lidar-based wind resource assessment and diagnostic surveys for wind farms.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <label>1</label><title>Introduction</title>
      <p id="d1e111">The use of Doppler light detection and ranging (lidar) technology for wind energy applications has largely increased over the last decade <xref ref-type="bibr" rid="bib1.bibx15 bib1.bibx61" id="paren.2"/>. Thanks to the achieved measurement accuracy and simpler and cost-effective deployments compared to traditional meteorological tower instrumentation, this remote sensing technique is now included in the international standards as a reliable tool for performance diagnostics of wind turbines and wind resource assessments <xref ref-type="bibr" rid="bib1.bibx28" id="paren.3"/>. Nonetheless, due to the limited spatiotemporal resolution and the distribution of the sample points in a spherical reference frame, the reconstruction of wind statistics from lidar samples still presents several challenges <xref ref-type="bibr" rid="bib1.bibx54 bib1.bibx48" id="paren.4"/>.</p>
      <p id="d1e123">In the companion paper <xref ref-type="bibr" rid="bib1.bibx42" id="paren.5"/>, we presented a revisited Barnes objective analysis <xref ref-type="bibr" rid="bib1.bibx5" id="paren.6"/> for the calculation of wind statistics from scattered lidar data, which is referred to as LiDAR Statistical Barnes Objective Analysis (LiSBOA). This procedure enables the estimation, over a Cartesian grid, of the mean, variance, and even higher-order central statistical moments of the radial velocity field probed by a scanning Doppler pulsed wind lidar. LiSBOA also performs adequate filtering of small-scale variability in the mean velocity field and mitigation of the dispersive stresses on the higher-order statistics, provided that the algorithm is tuned based on the characteristics of the flow under investigation and the free parameters of the lidar scan are optimally designed through LiSBOA.</p>
      <?pagebreak page2096?><p id="d1e132">LiSBOA's ability to estimate statistics of an ergodic turbulent velocity field makes it a suitable tool for the analysis of wind turbine wakes and the resource assessment of sites characterized by heterogeneous wind conditions, such as in presence of flow distortions induced by complex terrain. Over the last decade, wind lidars have been used to investigate wind turbine wakes; for instance, <xref ref-type="bibr" rid="bib1.bibx34" id="text.7"/> and <xref ref-type="bibr" rid="bib1.bibx16" id="text.8"/> measured the velocity deficit past utility-scale wind turbines, while <xref ref-type="bibr" rid="bib1.bibx10" id="text.9"/> used a nacelle-mounted lidar to detect wake displacements and validate the dynamic wake meandering model <xref ref-type="bibr" rid="bib1.bibx40" id="paren.10"/>. Fitting of the wake velocity deficit was successfully exploited to extract quantitative information about wake evolution from lidar measurements <xref ref-type="bibr" rid="bib1.bibx1 bib1.bibx64 bib1.bibx39 bib1.bibx58 bib1.bibx11" id="paren.11"/>.</p>
      <p id="d1e150">A deeper understanding of the physics of turbine wakes was achieved by calculating temporal <xref ref-type="bibr" rid="bib1.bibx57 bib1.bibx31 bib1.bibx29 bib1.bibx39 bib1.bibx44 bib1.bibx59" id="paren.12"/> or conditional <xref ref-type="bibr" rid="bib1.bibx4 bib1.bibx45 bib1.bibx22 bib1.bibx12 bib1.bibx32 bib1.bibx65 bib1.bibx66" id="paren.13"/> statistics of the velocity collected through lidar scans performed at different times. Using this approach, <xref ref-type="bibr" rid="bib1.bibx29" id="text.14"/> detected a significant dependence of the wake recovery rate on atmospheric stability, based on time-averaged volumetric lidar scans. The same concept was expanded by other authors using ensemble statistics <xref ref-type="bibr" rid="bib1.bibx45 bib1.bibx13 bib1.bibx65 bib1.bibx66" id="paren.15"/>. <xref ref-type="bibr" rid="bib1.bibx39" id="text.16"/> carried out a comparison between instantaneous, 10 min, and daily averaged velocity and turbulence intensity fields around utility-scale wind turbines, highlighting the presence of persistent turbulent wakes. <xref ref-type="bibr" rid="bib1.bibx57" id="text.17"/> used a nacelle-mounted lidar to quantify meandering-induced wake diffusion and added turbulence from statistics calculated over 10 min periods.</p>
      <p id="d1e173">Second-order statistics are of great interest in wind energy. <xref ref-type="bibr" rid="bib1.bibx31" id="text.18"/> used velocity time series extracted from lidar fixed scans performed downstream of a 2 <inline-formula><mml:math id="M1" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MW</mml:mi></mml:mrow></mml:math></inline-formula> wind turbine to detect enhanced turbulence intensity in the proximity of the wake shear layers. More recently, temporal statistics over 30 min periods allowed for the identification of turbulent wake shear layers from both numerical <xref ref-type="bibr" rid="bib1.bibx21" id="paren.19"/> and experimental <xref ref-type="bibr" rid="bib1.bibx13" id="paren.20"/> velocity fields. <xref ref-type="bibr" rid="bib1.bibx4" id="text.21"/> attempted to characterize the turbulence intensity using bin statistics, despite achieving higher values than expected, i.e., larger than 50 %. <xref ref-type="bibr" rid="bib1.bibx65" id="text.22"/> used clustered data of wake velocity fields to retrieve a proxy for the standard deviation of wind speed in the wake of utility-scale turbines. These authors reported significant variability in the wake turbulent statistics, depending on the atmospheric stability regime and operative conditions of the wind turbines.</p>
      <p id="d1e200">For the abovementioned technical features of lidars, these remote sensing instruments are now also used for wind resource assessment <xref ref-type="bibr" rid="bib1.bibx43" id="paren.23"/>, enabling estimates of wind statistics for broad ranges of wind conditions and site typology, such as for flat terrains <xref ref-type="bibr" rid="bib1.bibx33 bib1.bibx56 bib1.bibx53" id="paren.24"/>, complex terrains <xref ref-type="bibr" rid="bib1.bibx37 bib1.bibx38 bib1.bibx49 bib1.bibx35 bib1.bibx60 bib1.bibx33 bib1.bibx52 bib1.bibx46 bib1.bibx19" id="paren.25"/>, and near-shore <xref ref-type="bibr" rid="bib1.bibx26 bib1.bibx20 bib1.bibx55" id="paren.26"/> and off-shore locations <xref ref-type="bibr" rid="bib1.bibx50 bib1.bibx36 bib1.bibx23 bib1.bibx63" id="paren.27"/>. Lidar scanning strategies for wind resource assessment encompass Doppler beam swinging <xref ref-type="bibr" rid="bib1.bibx26 bib1.bibx49 bib1.bibx35 bib1.bibx55 bib1.bibx23 bib1.bibx63 bib1.bibx56 bib1.bibx53" id="paren.28"><named-content content-type="pre">DBS;</named-content></xref>, plan position indicator (PPI) scans <xref ref-type="bibr" rid="bib1.bibx37 bib1.bibx38 bib1.bibx49 bib1.bibx20 bib1.bibx60 bib1.bibx33" id="paren.29"/>, range height indicator (RHI) scans <xref ref-type="bibr" rid="bib1.bibx50 bib1.bibx20 bib1.bibx46 bib1.bibx19" id="paren.30"/>, or fixed scans <xref ref-type="bibr" rid="bib1.bibx52" id="paren.31"/>. Statistics are generally calculated based on the canonical 10 min periods, assuming steady inflow conditions, while linear interpolation is widely used for data postprocessing.</p>
      <p id="d1e233">In light of the great relevance for the wind energy applications of the statistical analysis of wind lidar data, for this work the LiSBOA procedure is applied to real lidar measurements of wind turbine wakes. The scope of this study is dual. First, there is an assessment of the capabilities provided by LiSBOA for the optimal selection of the angular step of the lidar scans by maximizing the statistical accuracy of the measurements and coverage of the sampling domain with the prescribed spatial resolution; second, the potential of LiSBOA to reconstruct mean velocity and turbulence intensity fields from lidar data to unveil important flow features of wind turbine wakes is shown.</p>
      <p id="d1e236">With these aims, real lidar data collected in the wakes generated by four 1.5 <inline-formula><mml:math id="M2" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MW</mml:mi></mml:mrow></mml:math></inline-formula> wind turbines are analyzed through LiSBOA. Specific wake features, such as the high-speed jet around the nacelle and the turbulent shear layers, as well as perturbations induced by the complex topography, are detected. Then, to provide a quantitative comparison with the data retrieved through traditional anemometers, LiSBOA is employed to calculate mean velocity and turbulence intensity fields of the wakes generated by four 1 <inline-formula><mml:math id="M3" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MW</mml:mi></mml:mrow></mml:math></inline-formula> turbines interacting with each other.</p>
      <p id="d1e255">The remainder of the paper is organized as follows: Sect. <xref ref-type="sec" rid="Ch1.S2"/> provides a description of the site and the experimental setup of the field campaign. In Sect. <xref ref-type="sec" rid="Ch1.S3"/>, the scan design and the reconstruction of the statistics of the noninteracting wakes are discussed, while Sect. <xref ref-type="sec" rid="Ch1.S4"/> presents the results of the comparison between nacelle anemometer statistics and LiSBOA for the multiple interacting wakes. Finally, conclusions are drawn in Sect. <xref ref-type="sec" rid="Ch1.S5"/>. The paper uses the symbols introduced in the companion paper <xref ref-type="bibr" rid="bib1.bibx42" id="text.32"/>, which the reader is encouraged to review for a better understanding of the present paper.</p>
</sec>
<?pagebreak page2097?><sec id="Ch1.S2">
  <label>2</label><title>Site description and experimental setup</title>
      <p id="d1e277">Lidar data collected during an experimental campaign carried out at an onshore wind farm are used to assess the potential of the LiSBOA algorithm for wind energy applications. The measurements were collected during a long-term experimental campaign conducted at a large wind farm located in northeastern Colorado (Fig. <xref ref-type="fig" rid="Ch1.F1"/>). This wind park encompasses 221 Mitsubishi 1-MW and 53 General Electric 1.5-MW wind turbines. More technical specifications of the wind turbines are provided in Table <xref ref-type="table" rid="Ch1.T1"/>.</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="d1e286">Map of the wind farm under investigation. <bold>(a)</bold> Top view of the wind farm, with the diameter of the dots representing the turbine rotor diameter (in the wind rose, the sectors where both meteorological (met) towers are potentially affected by turbine wakes are displayed in lighter color). <bold>(b)</bold> Area probed through StreamLine XR lidar on 11 and 12 October 2018. <bold>(c)</bold> Typical field of view of the WindCube 200S lidar.</p></caption>
        <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f01.png"/>

      </fig>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T1" specific-use="star"><?xmltex \currentcnt{1}?><label>Table 1</label><caption><p id="d1e307">Technical specifications of the wind turbines under investigation.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="3">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">MWT-1000-61</oasis:entry>
         <oasis:entry colname="col3">GE sle1.5</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">Rated power (<inline-formula><mml:math id="M4" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">kW</mml:mi></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">1000</oasis:entry>
         <oasis:entry colname="col3">1500</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Cut-in wind speed (<inline-formula><mml:math id="M5" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">3.5</oasis:entry>
         <oasis:entry colname="col3">3.5</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Cut-out wind speed (<inline-formula><mml:math id="M6" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">25</oasis:entry>
         <oasis:entry colname="col3">25</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Rated wind speed (<inline-formula><mml:math id="M7" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">13.5</oasis:entry>
         <oasis:entry colname="col3">14</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Type</oasis:entry>
         <oasis:entry colname="col2">Variable pitch and/or fixed speed</oasis:entry>
         <oasis:entry colname="col3">Variable pitch and/or variable speed</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Hub height (m)</oasis:entry>
         <oasis:entry colname="col2">69</oasis:entry>
         <oasis:entry colname="col3">80</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Rotor diameter (m)</oasis:entry>
         <oasis:entry colname="col2">61.4</oasis:entry>
         <oasis:entry colname="col3">77</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <p id="d1e483">The wind rose, based on 3 years of wind speed and direction measured by the two meteorological (met) towers present on the site, reveals a prevalence of northwesterly and southeasterly wind directions. A characteristic of this site is the presence of a steep escarpment, with an average jump in altitude of about 80 m, surrounding a relatively flat plateau where the turbines are installed.</p>
      <p id="d1e486">A total of two pulsed Doppler scanning wind lidars were deployed. A WindCube 200S manufactured by Leosphere (Fig. <xref ref-type="fig" rid="Ch1.F2"/>a) was installed for the period May–December 2018 in the southern part of the farm, with the scope of detecting turbine wakes and flow distortions induced by the topography. The lidar was connected to the University of Texas at Dallas (UTD) mobile lidar station <xref ref-type="bibr" rid="bib1.bibx17 bib1.bibx65" id="paren.33"/> for remote control, scan setup, and data acquisition. Furthermore, a StreamLine XR by HALO Photonics (Fig. <xref ref-type="fig" rid="Ch1.F2"/>b) was deployed for the period 11–19 October 2018 at specific sectors to investigate wake interactions and topography-related flow features. Additional details about the lidars, including the settings adopted for the present study, are provided in Table <xref ref-type="table" rid="Ch1.T2"/>.</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="d1e500">Photographs of the lidar experiment. <bold>(a)</bold> Lidar WindCube 200S and sonic anemometers (Campbell Scientific, Inc.; CSAT3). <bold>(b)</bold> Lidar StreamLine XR. <bold>(c)</bold> GE 1.5sle turbines of the B row.</p></caption>
        <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f02.png"/>

      </fig>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T2" specific-use="star"><?xmltex \currentcnt{2}?><label>Table 2</label><caption><p id="d1e521">Technical specifications and settings of the wind lidars deployed during the field campaign.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="3">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:thead>
       <oasis:row rowsep="1">
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">WindCube 200S</oasis:entry>
         <oasis:entry colname="col3">StreamLine XR</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1">Type</oasis:entry>
         <oasis:entry colname="col2">Pulsed – scanning</oasis:entry>
         <oasis:entry colname="col3">Pulsed – scanning</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Scanning mode</oasis:entry>
         <oasis:entry colname="col2">Continuous</oasis:entry>
         <oasis:entry colname="col3">Step stare</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Wavelength (<inline-formula><mml:math id="M8" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">nm</mml:mi></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">1543</oasis:entry>
         <oasis:entry colname="col3">1500</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Pulse length (<inline-formula><mml:math id="M9" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">ns</mml:mi></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">200</oasis:entry>
         <oasis:entry colname="col3">200</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Frequency (<inline-formula><mml:math id="M10" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">kHz</mml:mi></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">20</oasis:entry>
         <oasis:entry colname="col3">10</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Gate length (<inline-formula><mml:math id="M11" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">50</oasis:entry>
         <oasis:entry colname="col3">18</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Number of gates</oasis:entry>
         <oasis:entry colname="col2">80</oasis:entry>
         <oasis:entry colname="col3">200</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Rotation speed (<inline-formula><mml:math id="M12" display="inline"><mml:mrow class="unit"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2">1</oasis:entry>
         <oasis:entry colname="col3">0.85</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1">Detection range (<inline-formula><mml:math id="M13" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>)</oasis:entry>
         <oasis:entry colname="col2"><inline-formula><mml:math id="M14" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">30</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col3"><inline-formula><mml:math id="M15" display="inline"><mml:mrow><mml:mo>±</mml:mo><mml:mn mathvariant="normal">20</mml:mn></mml:mrow></mml:math></inline-formula></oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <p id="d1e745">The atmospheric stability is characterized through the Obukhov length <xref ref-type="bibr" rid="bib1.bibx47" id="paren.34"/> retrieved by two CSAT3 3D sonic anemometers manufactured by Campbell Scientific, Inc., which were deployed in the proximity of the UTD mobile lidar station at 1.4 and 2.8 m above the ground. A total of two met towers are installed in the northern part of the park, as shown in Fig. <xref ref-type="fig" rid="Ch1.F1"/>. Each tower is equipped with four anemometers installed in a paired configuration at heights of 50 and 80 m, for met tower no. 1, and 50 and 69 m, for met tower no. 2. Mean and standard deviation of wind speed and direction are stored every 10 min, along with the mean temperature and barometric pressure. In the present work, wind velocity data at each height are corrected for the flow distortion due to the tower following the guidelines provided by the International Electrotechnical Commission (IEC) standards <xref ref-type="bibr" rid="bib1.bibx28" id="paren.35"><named-content content-type="post">Annex G</named-content></xref>. Additionally, mean and standard deviation over 10 min periods of nacelle wind speed, power, revolutions per minute (RPM), and blade pitch, collected and stored by the supervisory control and data acquisition (SCADA) system, were made available. Normalized average power, <inline-formula><mml:math id="M16" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mtext>norm</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, and <inline-formula><mml:math id="M17" display="inline"><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mi mathvariant="normal">p</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> curves based on the nacelle anemometers are built by leveraging data for the period 2016–2018 and shown in Fig. <xref ref-type="fig" rid="Ch1.F3"/> as a function of the density-corrected normalized wind speed <xref ref-type="bibr" rid="bib1.bibx28" id="paren.36"/> as follows:
          <disp-formula id="Ch1.E1" content-type="numbered"><label>1</label><mml:math id="M18" display="block"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>norm</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>rated</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>⋅</mml:mo><mml:msup><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>met</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>ref</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:msup><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M19" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>ref</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1.225</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M20" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">kg</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">m</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> is the reference density at the sea level, <inline-formula><mml:math id="M21" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the 10 min average of the wind speed measured by the nacelle-mounted anemometers, while the local air density <inline-formula><mml:math id="M22" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ρ</mml:mi><mml:mtext>met</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is calculated from the meteorological data according to the international standard <xref ref-type="bibr" rid="bib1.bibx28" id="paren.37"/>. Another important parameter derived from the SCADA data is the turbulence intensity at the rotor, which is defined as follows:
          <disp-formula id="Ch1.E2" content-type="numbered"><label>2</label><mml:math id="M23" display="block"><mml:mrow><mml:msub><mml:mtext>TI</mml:mtext><mml:mtext>SCADA</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SD, SCADA</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M24" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SD, SCADA</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the standard deviation of wind speed over 10 min periods.</p>

      <?xmltex \floatpos{!h}?><fig id="Ch1.F3" specific-use="star"><?xmltex \currentcnt{3}?><?xmltex \def\figurename{Figure}?><label>Figure 3</label><caption><p id="d1e941">Performance curves for the General Electric (GE) and Mitsubishi (MHI) wind turbines. <bold>(a)</bold> Normalized power, <inline-formula><mml:math id="M25" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mtext>norm</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, and <bold>(b)</bold> power coefficient, <inline-formula><mml:math id="M26" display="inline"><mml:mrow><mml:msub><mml:mi>C</mml:mi><mml:mi mathvariant="normal">p</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f03.png"/>

      </fig>

      <p id="d1e978">The two lidars performed a great variety of scans during the campaign, based on the specific phenomena under investigation. For the present analysis, we focus on the 3D reconstruction of noninteracting wakes using the high-resolution data collected with the Halo StreamLine XR lidar and the 2D reconstruction of multiple overlapping wakes detected by the WindCube 200S.</p>
</sec>
<sec id="Ch1.S3">
  <label>3</label><title>Application of LiSBOA to volumetric lidar data</title>
      <p id="d1e989">This section aims to explore the potential of LiSBOA for the selection of the optimal azimuthal resolution of a lidar scan, data postprocessing, and reconstruction of 3D flow statistics. The data set used in this section was collected on 11 October 2018 over the farm region, shown in Fig. <xref ref-type="fig" rid="Ch1.F1"/>b, through a StreamLine XR lidar. The goal of the experiment is to investigate the evolution of multiple turbine wakes advected over complex terrain. Figure <xref ref-type="fig" rid="Ch1.F4"/> shows the site of the deployment and the relative distances between the lidar and the turbine hubs.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><?xmltex \currentcnt{4}?><?xmltex \def\figurename{Figure}?><label>Figure 4</label><caption><p id="d1e998">Satellite map of deployment of Halo StreamLine XR on 11 October 11 2018. Source: ©Google Maps.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f04.png"/>

      </fig>

      <?pagebreak page2098?><p id="d1e1007">The deployment location was chosen to scan the wakes generated by wind turbines B16–B19 for south-southeast (SSE) wind directions. The lidar was deployed off a county road that connects the plateau with the surrounding plains, with a consequent difference in altitude between the instrument and the base of the turbines of about 40 m. To probe the wake region of turbines B16–B19 (Fig. <xref ref-type="fig" rid="Ch1.F2"/>c) and the leeward side of the ridge, seven PPI scans were performed by sweeping an azimuthal range of 65<inline-formula><mml:math id="M27" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> with elevations angles, <inline-formula><mml:math id="M28" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula>, set to 5, 6, 7, 8, 10, 12, and 15<inline-formula><mml:math id="M29" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. The total sampling time was selected equal to <inline-formula><mml:math id="M30" display="inline"><mml:mrow><mml:mi>T</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> h, since the local weather forecast service provided by the wind farm operator predicted 1 h of steady wind conditions, blowing in a SSE mean direction and having a speed of <inline-formula><mml:math id="M31" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub><mml:mo>≈</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M32" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. The aerosol concentration allowed for the selection of a gate length of <inline-formula><mml:math id="M33" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>r</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">18</mml:mn></mml:mrow></mml:math></inline-formula> m and accumulation time of 1.2 s.</p>
      <p id="d1e1097">As reported in Sect. 4 of <xref ref-type="bibr" rid="bib1.bibx42" id="text.38"/>, several parameters of the flow under investigation are required for the optimal design of the lidar scans. The fundamental half wavelengths typical for wind turbine wakes were selected equal to those used in Sect. 5 of <xref ref-type="bibr" rid="bib1.bibx42" id="text.39"/>, i.e., <inline-formula><mml:math id="M34" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2.5</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M35" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>z</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.5</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula>. Similarly, the integral timescale was chosen equal to <inline-formula><mml:math id="M36" display="inline"><mml:mrow><mml:mi mathvariant="italic">τ</mml:mi><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:mi>D</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.4</mml:mn></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math id="M37" display="inline"><mml:mrow><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> s). Finally, a measurement volume with dimensions of 1000, 950, and 130 m in the streamwise, transverse, and vertical directions, respectively, was selected to probe wakes generated from turbines B16–B19 and the downwind region of the escarpment. The expected characteristic velocity standard deviation was estimated to be <inline-formula><mml:math id="M38" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.125</mml:mn><mml:mspace linebreak="nobreak" width="0.25em"/><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, based on previous field measurements of turbine wakes under stable conditions <xref ref-type="bibr" rid="bib1.bibx65" id="paren.40"/>.</p>
      <p id="d1e1234">For the selection of the optimal azimuthal angular resolution of the lidar scan, LiSBOA is applied to produce a Pareto front for six possible angular resolutions, <inline-formula><mml:math id="M39" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:math></inline-formula>, between 0.25 and 4<inline-formula><mml:math id="M40" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, and four values of the smoothing parameter, <inline-formula><mml:math id="M41" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mo>[</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">6</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">8</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">17</mml:mn><mml:mo>]</mml:mo></mml:mrow></mml:math></inline-formula>. As shown in Fig. <xref ref-type="fig" rid="Ch1.F5"/>, the optimal lidar scan is that with angular resolution <inline-formula><mml:math id="M42" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M43" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> or <inline-formula><mml:math id="M44" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula>. Generally, an increasing <inline-formula><mml:math id="M45" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:math></inline-formula> entails a reduction in the standard deviation of the mean, <inline-formula><mml:math id="M46" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mtext>II</mml:mtext></mml:msup></mml:mrow></mml:math></inline-formula>, yet values higher than <inline-formula><mml:math id="M47" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> do not lead to significant reductions in <inline-formula><mml:math id="M48" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mtext>II</mml:mtext></mml:msup></mml:mrow></mml:math></inline-formula>, while worsening the data loss, <inline-formula><mml:math id="M49" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mi mathvariant="normal">I</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula>, indicating a larger number of grid points not satisfying the Petersen–Middleton constraint.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5"><?xmltex \currentcnt{5}?><?xmltex \def\figurename{Figure}?><label>Figure 5</label><caption><p id="d1e1418">Pareto front for the design of the optimal lidar scan for the reconstruction of the wakes generated by wind turbines B16–B19. The markers highlighted in red correspond to the respective parameters obtained from the actual lidar data after the quality control process.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f05.png"/>

      </fig>

      <?pagebreak page2099?><p id="d1e1427">In Fig. <xref ref-type="fig" rid="Ch1.F5"/>, the values of the cost function <inline-formula><mml:math id="M50" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mi mathvariant="normal">I</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M51" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mtext>II</mml:mtext></mml:msup></mml:mrow></mml:math></inline-formula>, calculated from the lidar data after the quality control process <xref ref-type="bibr" rid="bib1.bibx8" id="paren.41"/>, are also reported for the optimal angular spacing of the lidar <inline-formula><mml:math id="M52" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>. It is noteworthy that there is a negligible difference between the values calculated before and after the quality control of the lidar data, indicating that the data loss due to the acquisition error is negligible in the domain of interest. The spatial distributions of the grid points satisfying the Petersen–Middleton constraint for different values of <inline-formula><mml:math id="M53" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M54" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> are reported in Fig. <xref ref-type="fig" rid="Ch1.F6"/>. It can be observed, as <inline-formula><mml:math id="M55" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> represents the highest angular step, ensuring an acceptable coverage of the spatial domain.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F6" specific-use="star"><?xmltex \currentcnt{6}?><?xmltex \def\figurename{Figure}?><label>Figure 6</label><caption><p id="d1e1524">Random data spacing, <inline-formula><mml:math id="M56" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mover accent="true"><mml:mi>d</mml:mi><mml:mo mathvariant="normal" stretchy="false">̃</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula>, for six volumetric scans with different angular resolution and <inline-formula><mml:math id="M57" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula>. Points violating the Petersen–Middleton constraint (<inline-formula><mml:math id="M58" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mover accent="true"><mml:mi>d</mml:mi><mml:mo stretchy="false" mathvariant="normal">̃</mml:mo></mml:mover><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>) are not displayed.</p></caption>
        <?xmltex \igopts{width=369.885827pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f06.png"/>

      </fig>

      <p id="d1e1580">The data collected, adopting the optimal scanning strategy with <inline-formula><mml:math id="M59" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>, are now postprocessed to calculate the mean streamwise velocity and turbulence intensity. The time series of the wind speed and direction recorded by the sensors installed on met tower no. 1 at hub height and located at a distance of 2700 <inline-formula><mml:math id="M60" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> in the northern direction of the test site are leveraged to characterize the incoming wind. The evolution of wind speed and direction along with the velocity field, measured with three specific PPI scans, are reported in Fig. <xref ref-type="fig" rid="Ch1.F7"/>. For the period between 20:30 and 21:30 local time (Mountain daylight time – MDT), and indicated by the shaded area in Fig. <xref ref-type="fig" rid="Ch1.F7"/>a and b, the wind speed remained within the range between 5.1 and 7.1 <inline-formula><mml:math id="M61" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, while the wind direction departed less than 10<inline-formula><mml:math id="M62" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> from its mean value of <inline-formula><mml:math id="M63" display="inline"><mml:mrow><mml:msub><mml:mover accent="true"><mml:mi mathvariant="italic">θ</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">163.4</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>. The wind and power data, which are recorded by SCADA (Fig. <xref ref-type="fig" rid="Ch1.F8"/>), confirm that the turbines experienced fairly homogeneous inflow<?pagebreak page2100?> conditions, with the differences in power capture being 5 % smaller than the rated value. The values of normalized velocity, together with the performance curves (Fig. <xref ref-type="fig" rid="Ch1.F3"/>), indicate that the turbines were operating in region II of the power curve for the whole interval of interest.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F7" specific-use="star"><?xmltex \currentcnt{7}?><?xmltex \def\figurename{Figure}?><label>Figure 7</label><caption><p id="d1e1668">3D lidar scans of five wind turbines. <bold>(a)</bold> The 10 min average wind speed measured from the anemometers installed at 50 and 80 m height on met tower no. 1. The error bar represents the standard deviation over 10 min. The shaded area represents the interval selected for the LiSBOA application. <bold>(b)</bold> The 10 min average wind direction in the geophysical reference system measured from the vanes installed at 50 and 80 m on met tower no. 1. <bold>(c–e)</bold> Equivalent velocity fields measured with PPI scans at different times. The green arrow is oriented as being the mean wind direction measured by met tower no. 1, while the black cross indicates the lidar location.</p></caption>
        <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f07.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8" specific-use="star"><?xmltex \currentcnt{8}?><?xmltex \def\figurename{Figure}?><label>Figure 8</label><caption><p id="d1e1688">SCADA data during the selected testing period. <bold>(a)</bold> Normalized hub height velocity. <bold>(b)</bold> Turbulence intensity. <bold>(c)</bold> Normalized power.</p></caption>
        <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f08.png"/>

      </fig>

      <p id="d1e1706">Since statistical stationarity is an important assumption for the LiSBOA applications, adequate postprocessing of the lidar data is needed to avoid effects on the reconstructed flow statistics due to the wind variability. Specifically, the wind speed variability is corrected by making the line-of-sight velocity nondimensional with the incoming wind speed. To this end, the instantaneous velocity field measured by the lidar is divided by the synchronized mean wind speed obtained from met tower no. 1, as explained above. Furthermore, scans performed when the wind direction was outside of the range <inline-formula><mml:math id="M64" display="inline"><mml:mrow><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>±</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:math></inline-formula>, with <inline-formula><mml:math id="M65" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">10</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>, are excluded. After the quality control based on the dynamic filtering <xref ref-type="bibr" rid="bib1.bibx8" id="paren.42"/>, 169 000 data points out of 455 000 are made available for the LiSBOA reconstruction on a Cartesian grid, with resolution equal to <inline-formula><mml:math id="M66" display="inline"><mml:mrow><mml:mi mathvariant="bold-italic">d</mml:mi><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="bold">Δ</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">n</mml:mi><mml:mn mathvariant="bold">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. Isolated grid regions violating the Petersen–Middleton constraint (<inline-formula><mml:math id="M67" display="inline"><mml:mrow><mml:mo>&lt;</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mi mathvariant="italic">%</mml:mi></mml:mrow></mml:math></inline-formula> of the total number of grid points) are rejected, and their respective values are filled through a Laplacian interpolation (inpaint_nans.m in MATLAB). This analysis is restricted to the streamwise component of the wind velocity, which is estimated using the equivalent velocity approach <xref ref-type="bibr" rid="bib1.bibx65" id="paren.43"/>. The nondimensional equivalent velocity is referred to as <inline-formula><mml:math id="M68" display="inline"><mml:mrow><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>/</mml:mo><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> in the remainder of the paper, while the associated turbulence intensity is referred to as <inline-formula><mml:math id="M69" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>/</mml:mo><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9" specific-use="star"><?xmltex \currentcnt{9}?><?xmltex \def\figurename{Figure}?><label>Figure 9</label><caption><p id="d1e1846">3D rendering of the normalized mean equivalent velocity field reconstructed with <inline-formula><mml:math id="M70" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">10</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>. The three isosurfaces represent <inline-formula><mml:math id="M71" display="inline"><mml:mrow><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>/</mml:mo><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.45</mml:mn></mml:mrow></mml:math></inline-formula>, 0.6, and 0.75, while the color maps represent cross sections of the mean velocity field over the respective planes reported in the rendering. The dashed circles correspond to the rotor-swept area of turbines B16–B19 (from left to right) projected onto the specific cross-plane.</p></caption>
        <?xmltex \igopts{width=398.338583pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f09.png"/>

      </fig>

      <?xmltex \floatpos{p}?><fig id="Ch1.F10" specific-use="star"><?xmltex \currentcnt{10}?><?xmltex \def\figurename{Figure}?><label>Figure 10</label><caption><p id="d1e1900">3D rendering of the turbulence intensity field reconstructed with <inline-formula><mml:math id="M72" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">10</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>. The two isosurfaces represent <inline-formula><mml:math id="M73" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>/</mml:mo><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula> levels of 20 % and 30 %, while the color maps represent cross sections of the turbulence intensity field over the respective planes reported in the rendering. The dashed circles correspond to the rotor-swept area of turbines B16–B19 (from left to right) projected onto the specific cross-plane.</p></caption>
        <?xmltex \igopts{width=398.338583pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f10.png"/>

      </fig>

      <p id="d1e1956">Figures <xref ref-type="fig" rid="Ch1.F9"/> and <xref ref-type="fig" rid="Ch1.F10"/> show 3D renderings of the nondimensional velocity and turbulence intensity fields obtained by using the parameters <inline-formula><mml:math id="M74" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> – <inline-formula><mml:math id="M75" display="inline"><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula>. Wake features, such as turbulent diffusion, the high-momentum jet in the hub region, and the turbulent shear layer at the wake boundary, are well-captured. A total of two highly turbulent regions are located on both sides of the wakes, which is a distinctive signature of wake meandering occurring mostly horizontally in the atmospheric boundary layer <xref ref-type="bibr" rid="bib1.bibx18" id="paren.44"><named-content content-type="pre">ABL;</named-content></xref>. The lack of symmetry and similarity among different turbines, however, suggests that full statistical convergence is not achieved on the second-order statistics for the available data set. The low-speed region hovering over the downslope most probably represents the upper part of the low momentum zone that occurs past sharp escarpments <xref ref-type="bibr" rid="bib1.bibx9" id="paren.45"/>.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F11" specific-use="star"><?xmltex \currentcnt{11}?><?xmltex \def\figurename{Figure}?><label>Figure 11</label><caption><p id="d1e2002">Comparison of the turbulence intensity reconstructed with <inline-formula><mml:math id="M76" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> – <inline-formula><mml:math id="M77" display="inline"><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> <bold>(a, b, c)</bold> vs. <inline-formula><mml:math id="M78" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula> – <inline-formula><mml:math id="M79" display="inline"><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:math></inline-formula> <bold>(d, e, f)</bold> and their difference <bold>(g, h, i)</bold> for three selected streamwise locations indicated by the red lines in the top maps.</p></caption>
        <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-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="d1e2080">Rotor-averaged streamwise mean velocity and turbulence intensity as a function of the downstream distance from the turbine and associated altitude profile.</p></caption>
        <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f12.png"/>

      </fig>

      <?pagebreak page2102?><p id="d1e2089">The effect of the combination <inline-formula><mml:math id="M80" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula> – <inline-formula><mml:math id="M81" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula> on higher-order statistics is investigated by extracting the turbulence intensity at different cross-stream planes. The optimal pairs <inline-formula><mml:math id="M82" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>-</mml:mo><mml:mi>m</mml:mi></mml:mrow></mml:math></inline-formula> identified by the Pareto front analysis (Fig. <xref ref-type="fig" rid="Ch1.F5"/>), namely <inline-formula><mml:math id="M83" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mo>-</mml:mo><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M84" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">6</mml:mn><mml:mo>-</mml:mo><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:math></inline-formula>, are tested here. One may expect that, due to the difference in the response of the high-order moments of the fundamental mode between the two pairs, <inline-formula><mml:math id="M85" display="inline"><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msup><mml:mo>(</mml:mo><mml:mi mathvariant="bold">Δ</mml:mi><mml:msub><mml:mover accent="true"><mml:mi mathvariant="bold-italic">n</mml:mi><mml:mo mathvariant="normal" stretchy="false">̃</mml:mo></mml:mover><mml:mn mathvariant="bold">0</mml:mn></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>, the first case would exhibit a significantly lower <inline-formula><mml:math id="M86" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>/</mml:mo><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula> with respect to the second one. However, as shown in Fig. <xref ref-type="fig" rid="Ch1.F11"/>, the peaks of turbulence intensity are quite similar between the two cases. The main difference between the two reconstruction processes is a smoother distribution of <inline-formula><mml:math id="M87" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>/</mml:mo><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula> for <inline-formula><mml:math id="M88" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mo>-</mml:mo><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula>. The similarity between the two cases is due, essentially, to the following two reasons: first, the smallest energy-containing length scales of the turbulence intensity field (i.e., shear layer thickness) are larger than the selected fundamental mode <inline-formula><mml:math id="M89" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>z</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.5</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula>; second, the larger number of points per grid node averaged for the <inline-formula><mml:math id="M90" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> case, leads to a higher variance due to the reduction in the bias of the estimator of the variance, which partially compensates the lower theoretical response. In summary, this sensitivity analysis suggests that the choice of the <inline-formula><mml:math id="M91" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>-</mml:mo><mml:mi>m</mml:mi></mml:mrow></mml:math></inline-formula> pair cannot be based purely on the theoretical response, since it does not take into account the nonideal effects deriving from the discrete and nonuniform data distribution. Instead, an a posteriori analysis of the statistics retrieved is recommended to select the best <inline-formula><mml:math id="M92" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>-</mml:mo><mml:mi>m</mml:mi></mml:mrow></mml:math></inline-formula> values.</p>
      <p id="d1e2351">Turbine-wake statistics are extremely sensitive to the width of the selected wind sector <xref ref-type="bibr" rid="bib1.bibx6 bib1.bibx24" id="paren.46"/>. It is well known that widening the wind direction range can lead to an enhanced wake diffusion and turbulence intensity <xref ref-type="bibr" rid="bib1.bibx57 bib1.bibx39" id="paren.47"/>, which is compensated by higher data availability and statistical significance. A sensitivity analysis to the wind sector width for reconstructing the statistics through LiSBOA for two additional values of <inline-formula><mml:math id="M93" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is now presented. Besides the baseline value of 10<inline-formula><mml:math id="M94" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, the effects of a narrower (<inline-formula><mml:math id="M95" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>) and wider (<inline-formula><mml:math id="M96" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">15</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>) range are investigated. The standard deviation of the wind direction associated with the different sectors is 1.08, 1.93, and 2.74<inline-formula><mml:math id="M97" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> for <inline-formula><mml:math id="M98" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">5</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">10</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">15</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula>, respectively. Figure <xref ref-type="fig" rid="Ch1.F12"/> shows the rotor-averaged velocity and turbulence intensity for each turbine as a function of the downstream distance from the rotor. The profiles of the mean and standard deviation obtained for different <inline-formula><mml:math id="M99" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are practically the same, indicating that the effects of the wind direction variability on wake flow statistics are not significant.</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="d1e2480">Fields reconstructed adopting several <inline-formula><mml:math id="M100" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> values and sampled at <inline-formula><mml:math id="M101" display="inline"><mml:mrow><mml:mi>x</mml:mi><mml:mo>/</mml:mo><mml:mi>D</mml:mi><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">1.3</mml:mn></mml:mrow></mml:math></inline-formula> downstream of turbines B16, B17, B18, and B19. <bold>(a)</bold> Mean streamwise velocity and <bold>(b)</bold> streamwise turbulence intensity.</p></caption>
        <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f13.png"/>

      </fig>

      <p id="d1e2524">For the sake of completeness, the velocity and turbulence intensity sampled in the cross-stream plane, where the maximum velocity deficit occurs (<inline-formula><mml:math id="M102" display="inline"><mml:mrow><mml:mi>x</mml:mi><mml:mo>/</mml:mo><mml:mi>D</mml:mi><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">1.3</mml:mn></mml:mrow></mml:math></inline-formula>), for all the turbines and the <inline-formula><mml:math id="M103" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are shown in Fig. <xref ref-type="fig" rid="Ch1.F13"/>. The discrepancies due to different <inline-formula><mml:math id="M104" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are negligible. A more evident mismatch can be observed in the shape of the wakes among different wind turbines, with the wake of turbine B19, in particular, showing the velocity deficit and turbulence peak that are displaced above the hub height. Turbine B19 is also the only one facing a slightly inclined terrain (see Fig. <xref ref-type="fig" rid="Ch1.F12"/>), which may have caused a skewed inflow.</p>
</sec>
<sec id="Ch1.S4">
  <label>4</label><title>Application of LiSBOA to interacting wind turbine wakes</title>
      <p id="d1e2581">An assessment of the accuracy of LiSBOA in the calculation of mean wind speed and turbulence intensity is now provided for lidar measurements performed during the occurrence of wake interactions. To this end, point-wise measurements provided by the nacelle-mounted anemometers and saved in the SCADA data of four closely spaced Mitsubishi wind turbines, roughly aligned with the wind direction, are compared with the statistics obtained from the postprocessing of the lidar data with LiSBOA.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F14"><?xmltex \currentcnt{14}?><?xmltex \def\figurename{Figure}?><label>Figure 14</label><caption><p id="d1e2586">Satellite map of the site for the deployment of the WindCube 200S lidar, including the four Mitsubishi wind turbines under investigation. Source: ©Google Maps.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f14.png"/>

      </fig>

      <p id="d1e2595">Figure <xref ref-type="fig" rid="Ch1.F14"/> reports a satellite image of the site used in this experiment. The tests were performed during the occurrence of a nearly steady northeasterly wind (<inline-formula><mml:math id="M105" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">8</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math id="M106" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>) from 21:00 to 01:00 local time (<inline-formula><mml:math id="M107" display="inline"><mml:mrow><mml:mi>T</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> h) in the night between 5 and 6 September 2018. This wind condition created<?pagebreak page2103?> a good alignment of the wakes emitted by the turbines F01 to F04. The aerosol conditions allowed us to run the WindCube 200S lidar with a gate length of 50 m and an accumulation time of 0.5 s. The lidar is located at a distance of about <inline-formula><mml:math id="M108" display="inline"><mml:mrow><mml:mn mathvariant="normal">25</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> from wind turbine F04, which is the most downstream turbine for that specific wind condition, while the average streamwise spacing between the turbines is <inline-formula><mml:math id="M109" display="inline"><mml:mrow><mml:mn mathvariant="normal">3.6</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula>. The velocity and turbulence intensity fields are reconstructed over a horizontal plane, including only points within the vertical range spanning from the bottom-tip to the top-tip of the turbine rotors. The 2D reconstruction adopted here implies that a uniform weight is applied for points displaced at different <inline-formula><mml:math id="M110" display="inline"><mml:mi>z</mml:mi></mml:math></inline-formula>, which means the reconstructed statistics represent time-averaged and vertically averaged fields. This 2D approach is deemed convenient for the comparison with point-wise measurements recorded by SCADA through nacelle-mounted instruments as it represents an average of the wind characteristics over the rotor.</p>
      <p id="d1e2673">The region of interest was probed through a volumetric scan consisting of three PPI scans with elevation angles <inline-formula><mml:math id="M111" display="inline"><mml:mrow><mml:mi mathvariant="italic">β</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2.1</mml:mn></mml:mrow></mml:math></inline-formula>, 2.6, and 3.3<inline-formula><mml:math id="M112" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>. The fundamental half wavelengths were selected as <inline-formula><mml:math id="M113" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>x</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2.25</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M114" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>n</mml:mi><mml:mrow><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:mi>y</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.75</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula>. According to the previous cases, the integral timescale was estimated to be <inline-formula><mml:math id="M115" display="inline"><mml:mrow><mml:mi mathvariant="italic">τ</mml:mi><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:mi>D</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.4</mml:mn></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math id="M116" display="inline"><mml:mrow><mml:mi mathvariant="italic">τ</mml:mi><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> s). The characteristic velocity standard deviation was set to <inline-formula><mml:math id="M117" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.2</mml:mn><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. The value of the associated turbulence intensity is higher than that used for nonoverlapping wakes to account for the turbulence build-up, which is known to occur for turbines operating experiencing wake interactions <xref ref-type="bibr" rid="bib1.bibx14 bib1.bibx30" id="paren.48"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F15" specific-use="star"><?xmltex \currentcnt{15}?><?xmltex \def\figurename{Figure}?><label>Figure 15</label><caption><p id="d1e2812">Probability density functions of met and SCADA data recorded from 21:00 to 01:00 MDT in the night between 5 and 6 September 2018. <bold>(a)</bold> Wind speed from met towers. <bold>(b)</bold> Wind direction from met towers. <bold>(c)</bold> Inverse Obukhov length from our sonic anemometers. <bold>(d)</bold> Normalized wind speed from SCADA. <bold>(e)</bold> Turbulence intensity from SCADA. <bold>(f)</bold> Normalized power from SCADA.</p></caption>
        <?xmltex \igopts{width=455.244094pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f15.png"/>

      </fig>

      <p id="d1e2840">The incoming wind is characterized by averaging measurements collected from all the anemometers and wind vanes installed on both met towers, which are located 12 and 10.4 <inline-formula><mml:math id="M118" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">km</mml:mi></mml:mrow></mml:math></inline-formula> away from the leading turbine F01 (Fig. <xref ref-type="fig" rid="Ch1.F15"/>). The Obukhov length is calculated from both sonic anemometers, indicating a stable stratification regime. The SCADA data exhibit the typical signature of multiple wake interactions with reduced wind speed and power for downstream turbines, while turbulence intensity is enhanced, in particular for the F02 and F04 wind turbines.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F16"><?xmltex \currentcnt{16}?><?xmltex \def\figurename{Figure}?><label>Figure 16</label><caption><p id="d1e2855">Pareto front for the design of the optimal lidar scan for the reconstruction of the wakes statistics for turbines F01–F04. The markers highlighted in red represent the actual lidar data after quality control.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f16.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F17" specific-use="star"><?xmltex \currentcnt{17}?><?xmltex \def\figurename{Figure}?><label>Figure 17</label><caption><p id="d1e2867">Velocity statistics of the wakes generated by turbines F01–F04 reconstructed over the horizontal plane at hub height. <bold>(a)</bold> Mean streamwise velocity and <bold>(b)</bold> streamwise turbulence intensity. The black dots indicate the sampling locations used for the estimation of the incoming flow for the respective turbine.</p></caption>
        <?xmltex \igopts{width=426.791339pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f17.png"/>

      </fig>

      <?pagebreak page2105?><p id="d1e2882">The optimal design of the lidar scan is performed, considering six values of <inline-formula><mml:math id="M119" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:math></inline-formula> and four values of <inline-formula><mml:math id="M120" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula>. The obtained Pareto front is shown in Fig. <xref ref-type="fig" rid="Ch1.F16"/>, which indicates <inline-formula><mml:math id="M121" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.5</mml:mn><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M122" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn><mml:mo>,</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:math></inline-formula> or <inline-formula><mml:math id="M123" display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula> as the optimal scanning parameters. The equivalent velocity retrieved by the lidar is made nondimensional with the free stream velocity provided by the met towers. The wind direction range is set to <inline-formula><mml:math id="M124" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi mathvariant="italic">θ</mml:mi><mml:mi mathvariant="normal">w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">10</mml:mn></mml:mrow></mml:math></inline-formula><inline-formula><mml:math id="M125" display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>, resulting in a total measuring period of 150 min. Data points lying above the top-tip or below the bottom-tip heights are excluded for this data analysis. The dynamic filter technique is used to reject corrupted lidar data, producing a total of 544 000 quality controlled lidar samples over 1 327 000 collected lidar data within the selected wind direction range.</p>
      <p id="d1e2984">LiSBOA is carried out on a grid with resolution <inline-formula><mml:math id="M126" display="inline"><mml:mrow><mml:mi mathvariant="bold-italic">d</mml:mi><mml:mi mathvariant="bold-italic">x</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.25</mml:mn><mml:mi mathvariant="bold">Δ</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">n</mml:mi><mml:mn mathvariant="bold">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, using the combination smoothing parameters – number of iterations <inline-formula><mml:math id="M127" display="inline"><mml:mrow><mml:mi mathvariant="italic">σ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula> – <inline-formula><mml:math id="M128" display="inline"><mml:mrow><mml:mi>m</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>, which is, among the allowable combinations, the one providing the largest response of the higher-order moments. The obtained velocity and turbulence intensity fields over the horizontal plane at hub height are displayed in Fig. <xref ref-type="fig" rid="Ch1.F17"/>. The velocity deficit of F02 appears slightly larger than that detected behind the unwaked turbine F01, which is most probably due to the wake superimposition. An even deeper velocity deficit can be observed behind F03, which operates in a partially waked condition for this specific wind direction. Downstream of the third turbine, the wake deficit build-up saturates, confirming results from previous studies on close wake interactions <xref ref-type="bibr" rid="bib1.bibx7 bib1.bibx14" id="paren.49"/>. Finally, the relatively fast recovery of the wake of the trailing turbine, F04, can be ascribed to the enhanced mixing due to the wake-generated turbulence. Indeed, Fig. <xref ref-type="fig" rid="Ch1.F17"/>b shows significant wake-generated turbulence increasing past the leading turbine that reaches its maximum at a distance of <inline-formula><mml:math id="M129" display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> downstream of the rotor of F03. Interestingly, wake-generated turbulence is concentrated on the sides of the wake of F01, which experiences undisturbed flow, while it spreads around the whole wake region for the downstream turbines. This feature might be related to the presence of coherent wake vorticity structures in the near wake of turbine F01 <xref ref-type="bibr" rid="bib1.bibx30 bib1.bibx62 bib1.bibx3" id="paren.50"/>, while, further downstream, the perturbed inflow promotes the breakdown of such coherent structures, leading to more<?pagebreak page2106?> homogeneous turbulence. Finally, the large velocity deficit and/or high turbulence detected in the wake of F03 may be a consequence of the mentioned partial wake interaction, which exposes the rotor to a nonhomogeneous flow, resulting in a severely off-design operation.</p>
      <p id="d1e3057">From a more quantitative standpoint, the incoming wind conditions experienced by each turbine are characterized to perform a direct comparison with the nacelle anemometer data. To this aim, the mean velocity and turbulence intensity profiles are extracted from the lidar statistics at a distance of <inline-formula><mml:math id="M130" display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> upstream of the rotors over a segment spanning the whole rotor diameter. The sampling location is chosen based on previous studies <xref ref-type="bibr" rid="bib1.bibx51 bib1.bibx25" id="paren.51"/>, since <inline-formula><mml:math id="M131" display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> is generally considered the minimum distance upstream of the rotor where the influence of the induction zone can be neglected for normal operative conditions. The averaged values of <inline-formula><mml:math id="M132" display="inline"><mml:mrow><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>/</mml:mo><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M133" display="inline"><mml:mrow><mml:msqrt><mml:mover accent="true"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:msqrt><mml:mo>/</mml:mo><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:mrow></mml:math></inline-formula> of each upstream profile are then used for the comparison with the respective values recorded through SCADA.</p>
      <p id="d1e3127">A well-posed comparison of the wind statistics obtained from LiSBOA, SCADA, and met data requires two important elements. First, the statistical moments compared have to be equivalent; second, both the LiSBOA and SCADA data must be representative of the free stream conditions experienced by each turbine.</p>
      <p id="d1e3130">Regarding the first issue, the mean field obtained through LiSBOA, <inline-formula><mml:math id="M134" display="inline"><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula>, can be expressed as follows:
          <disp-formula id="Ch1.E3" content-type="numbered"><label>3</label><mml:math id="M135" display="block"><mml:mrow><mml:msub><mml:mfenced open="〈" close="〉"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mi>u</mml:mi><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mi>T</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mfenced close="〉" open="〈"><mml:mrow><mml:msub><mml:mfenced open="〈" close="〉"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mi>u</mml:mi><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover></mml:msub></mml:mrow></mml:mfenced><mml:mi>T</mml:mi></mml:msub><mml:mo>∼</mml:mo><mml:msub><mml:mfenced close="〉" open="〈"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>met</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mi>T</mml:mi></mml:msub><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math id="M136" display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mo>.</mml:mo><mml:msub><mml:mo>〉</mml:mo><mml:mi>T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the average calculated over the whole sampling period of 150 min, while <inline-formula><mml:math id="M137" display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mo>.</mml:mo><mml:msub><mml:mo>〉</mml:mo><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover></mml:msub></mml:mrow></mml:math></inline-formula> is the 10 min average performed by SCADA and the met tower acquisition system. <inline-formula><mml:math id="M138" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M139" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>met</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> are the 10 min averaged velocities recorded from SCADA and the met tower, respectively, while the symbol <inline-formula><mml:math id="M140" display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> indicates statistical equivalence.</p>
      <p id="d1e3273">Similarly, for the comparison between the velocity variance calculated through LiSBOA and the respective values recorded through SCADA, we have the following relationship:

              <disp-formula id="Ch1.E4" content-type="numbered"><label>4</label><mml:math id="M141" display="block"><mml:mrow><mml:mstyle class="stylechange" displaystyle="true"/><mml:mtable class="split" columnspacing="1em" rowspacing="0.2ex" displaystyle="true" columnalign="right left"><mml:mtr><mml:mtd><mml:mrow><mml:msub><mml:mfenced close="〉" open="〈"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mi>T</mml:mi></mml:msub></mml:mrow></mml:mtd><mml:mtd><mml:mrow><mml:mo>=</mml:mo><mml:msub><mml:mfenced close="〉" open="〈"><mml:mrow><mml:msub><mml:mfenced close="〉" open="〈"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover><mml:mrow><mml:mo>′</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover></mml:msub></mml:mrow></mml:mfenced><mml:mi>T</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mfenced close="〉" open="〈"><mml:mrow><mml:msubsup><mml:mfenced close="〉" open="〈"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mi>u</mml:mi><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfenced><mml:mi>T</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msubsup><mml:mfenced open="〈" close="〉"><mml:mrow><mml:msub><mml:mfenced open="〈" close="〉"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mi>u</mml:mi><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo mathvariant="normal" stretchy="false">^</mml:mo></mml:mover></mml:msub></mml:mrow></mml:mfenced><mml:mi>T</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mo>∼</mml:mo><mml:msub><mml:mfenced close="〉" open="〈"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mtext>SD, SCADA</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mtext>met</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mi>T</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mfenced open="〈" close="〉"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mtext>met</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mi>T</mml:mi></mml:msub></mml:mrow></mml:mtd></mml:mtr><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:mo>-</mml:mo><mml:msubsup><mml:mfenced close="〉" open="〈"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>met</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced><mml:mi>T</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mtr></mml:mtable></mml:mrow></mml:math></disp-formula>

        where <inline-formula><mml:math id="M142" display="inline"><mml:mrow><mml:msup><mml:mi>u</mml:mi><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math id="M143" display="inline"><mml:mrow><mml:msup><mml:mover accent="true"><mml:mi>u</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> are the velocity fluctuations with zero mean calculated over the period <inline-formula><mml:math id="M144" display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> and <inline-formula><mml:math id="M145" display="inline"><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover></mml:math></inline-formula>, respectively. The parameter <inline-formula><mml:math id="M146" display="inline"><mml:mrow><mml:msubsup><mml:mi>U</mml:mi><mml:mtext>SD, SCADA</mml:mtext><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:math></inline-formula> is the velocity variance recorded by SCADA over the period <inline-formula><mml:math id="M147" display="inline"><mml:mover accent="true"><mml:mi>T</mml:mi><mml:mo stretchy="false" mathvariant="normal">^</mml:mo></mml:mover></mml:math></inline-formula> of 10 min.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F18"><?xmltex \currentcnt{18}?><?xmltex \def\figurename{Figure}?><label>Figure 18</label><caption><p id="d1e3548">Met tower and turbines selected for the nacelle transfer function estimation. The directions highlighted in gray represent the valid wind sectors unaffected by turbine wake interactions. The dashed circles bound the allowed range of distances from the tower in compliance with IEC standard 61400-12-1 <xref ref-type="bibr" rid="bib1.bibx28" id="paren.52"/>.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f18.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F19" specific-use="star"><?xmltex \currentcnt{19}?><?xmltex \def\figurename{Figure}?><label>Figure 19</label><caption><p id="d1e3562">Nacelle transfer function for mean <bold>(a)</bold> and standard deviation <bold>(b)</bold> of wind speed. The error bars represent the standard error on the mean with 95 % confidence level.</p></caption>
        <?xmltex \igopts{width=384.112205pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f19.png"/>

      </fig>

      <?pagebreak page2107?><p id="d1e3577">To ensure that the SCADA mean and standard deviation of velocity are representative of the undisturbed wind conditions at each rotor, these velocity statistics are corrected for the flow distortion induced by the turbine through appropriate nacelle transfer functions (NTFs), which convert the velocity statistics measured at the nacelle of a wind turbine to the corresponding free stream values measured from a met tower located nearby. The IEC standard 61400-12-2 <xref ref-type="bibr" rid="bib1.bibx27" id="paren.53"/> prescribes the calculations of the NTF from the bin average, with bin size 0.5 <inline-formula><mml:math id="M148" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>, of the velocity measured by a reference anemometer as a function of the nacelle wind speed. In the present work, besides correcting the mean wind speed as indicated by the IEC standards, a linear correction of the wind speed standard deviation is also applied, as suggested by <xref ref-type="bibr" rid="bib1.bibx2" id="text.54"/>. We adopted, as reference, an anemometer that is installed at 69 m above the ground on met tower no. 2. The SCADA data of Mitsubishi turbines H05 and H06, both falling in the range of distances from the met tower recommended by the IEC 61400-12-1 <xref ref-type="bibr" rid="bib1.bibx28" id="paren.55"/>, are used. Only the unwaked wind sectors calculated based on the same standard are considered. The described layout is shown in Fig. <xref ref-type="fig" rid="Ch1.F18"/>, while Fig. <xref ref-type="fig" rid="Ch1.F19"/> shows the result of this analysis. There is a high correlation between the velocity measured by the met tower and the nacelle-mounted anemometer (<inline-formula><mml:math id="M149" display="inline"><mml:mrow><mml:mi mathvariant="italic">ρ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.976</mml:mn></mml:mrow></mml:math></inline-formula>). Nevertheless, the NTF of the velocity reveals consistently lower values occurring at the nacelle compared to the met tower, with a peak at 20 <inline-formula><mml:math id="M150" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">m</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">s</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. Concerning the standard deviation of velocity, the agreement between the SCADA and met tower data is significantly lower (<inline-formula><mml:math id="M151" display="inline"><mml:mrow><mml:mi mathvariant="italic">ρ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0.828</mml:mn></mml:mrow></mml:math></inline-formula>), yet a linear correction can be still calculated with acceptable significance (error on slope and intercept are 0.0038 and 0.0034, with 95 % confidence).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F20" specific-use="star"><?xmltex \currentcnt{20}?><?xmltex \def\figurename{Figure}?><label>Figure 20</label><caption><p id="d1e3655">Comparison between LiSBOA and SCADA wind statistics for a case with wake interactions. <bold>(a)</bold> Mean streamwise velocity normalized by free stream velocity. <bold>(b)</bold> Streamwise turbulence intensity.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f20.png"/>

      </fig>

      <p id="d1e3670">The results of the comparison between LiSBOA and SCADA are provided in Fig. <xref ref-type="fig" rid="Ch1.F20"/>. The mean velocity is accurately captured and confirms that F02 and F04 are the turbines mainly affected by the upstream wakes. The slightly higher momentum impinging F03 is mostly due to the imperfect alignment of that rotor with the upstream turbine wakes, which creates a condition of partial wake interaction. A slightly larger discrepancy between LiSBOA and SCADA data is observed for the turbulence intensity, with a maximum difference of <inline-formula><mml:math id="M152" display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> % for F03. Nonetheless, the main trend is well reproduced, and the overall agreement is satisfactory. The observed difference in turbulence intensity can be related to several factors, such as turbulence damping due to the lidar-measuring process and LiSBOA calculations, the accuracy of the NTF, the estimate of the streamwise velocity from the lidar radial velocity, or the vertical dispersive stresses.</p>
      <p id="d1e3685">The effect of the sampling location upstream of the turbines in the LiSBOA field is investigated by quantifying the discrepancy of the LiSBOA statistics with respect to the reference SCADA values for all the turbines through the 95th percentile of the absolute error, <inline-formula><mml:math id="M153" display="inline"><mml:mrow><mml:msub><mml:mtext>AE</mml:mtext><mml:mn mathvariant="normal">95</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. Figure <xref ref-type="fig" rid="Ch1.F21"/> shows <inline-formula><mml:math id="M154" display="inline"><mml:mrow><mml:msub><mml:mtext>AE</mml:mtext><mml:mn mathvariant="normal">95</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> as a function of the distance upstream, where the incoming flow is extracted from the LiSBOA statistics. For the mean velocity, it is confirmed that the value suggested by the literature (<inline-formula><mml:math id="M155" display="inline"><mml:mrow><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula>) is sufficiently far from the rotor to limit the effects of the induction zone on the definition of the reference free stream velocity. Furthermore, the rotor thrust does not seem to have noticeable effects on the incoming turbulence, in that the induction zone is essentially devoid of significant turbulent fluctuations due to the loads of the turbine blades. The discrepancy between the turbulence intensity retrieved through LiSBOA and SCADA steeply increases for sampling locations further than <inline-formula><mml:math id="M156" display="inline"><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> from the rotor.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F21"><?xmltex \currentcnt{21}?><?xmltex \def\figurename{Figure}?><label>Figure 21</label><caption><p id="d1e3740"><inline-formula><mml:math id="M157" display="inline"><mml:mrow><mml:msub><mml:mtext>AE</mml:mtext><mml:mn mathvariant="normal">95</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> of mean velocity and turbulence intensity for F01–F04 as a function of the upstream sampling location of the LiSBOA fields.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://amt.copernicus.org/articles/14/2095/2021/amt-14-2095-2021-f21.png"/>

      </fig>

      <p id="d1e3759">In summary, the satisfactory agreement between LiSBOA and SCADA data achieved in the present study indicates the proposed procedure as a promising candidate for wind resource assessment, especially for complex terrains, and investigations of the intra-wind-farm flow.</p>
</sec>
<?pagebreak page2108?><sec id="Ch1.S5" sec-type="conclusions">
  <label>5</label><title>Conclusions</title>
      <p id="d1e3771">The LiDAR Statistical Barnes Objective Analysis (LiSBOA) has been applied to two different cases of wind turbine wakes to estimate the optimal azimuthal step of the lidar and retrieve mean velocity and turbulence intensity fields.</p>
      <p id="d1e3774">First, LiSBOA has been used to process real lidar data collected for a utility-scale wind farm. For the first test case, the statistics of the wakes of four noninteracting 1.5 <inline-formula><mml:math id="M158" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MW</mml:mi></mml:mrow></mml:math></inline-formula> turbines placed at the brink of an escarpment have been reconstructed. The optimal azimuthal resolution of the lidar scan has been selected through LiSBOA, while the mean velocity and turbulence intensity fields retrieved through LiSBOA have offered a detailed insight of the wake morphology. Furthermore, a sensitivity analysis of the wind direction range has confirmed the robustness of the data selection and quality control methods.</p>
      <p id="d1e3785">Subsequently, the complex velocity field arising from the interaction of four 1 <inline-formula><mml:math id="M159" display="inline"><mml:mrow class="unit"><mml:mi mathvariant="normal">MW</mml:mi></mml:mrow></mml:math></inline-formula> turbines has been analyzed by calculating first- and second-order moments on the horizontal plane. The mean velocity and turbulence intensity extracted <inline-formula><mml:math id="M160" display="inline"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mi>D</mml:mi></mml:mrow></mml:math></inline-formula> upstream of the rotors have agreed well with the values provided by the nacelle anemometers, with maximum discrepancies as low as 3 % of the undisturbed wind speed for the mean velocity and 3 % (in absolute terms) for the turbulence intensity.</p>
      <p id="d1e3806">The applications of LiSBOA discussed in this work aim to showcase the potential of the proposed procedure for the optimal design of lidar scans and to provide guidelines for the utilization of LiSBOA for the analysis of lidar data. A total of two noticeable advantages of LiSBOA arise from the present work. First, once the wavelengths of interest and the lidar basic scanning parameters dictated by the atmospheric conditions and target position are selected, LiSBOA allows a systematic and effective optimization of the azimuthal resolution, which includes all the essential information of the flow under investigation and the lidars used. This feature can be of interest, especially when planning field experiments that involve multiple lidars, complex topography, or articulated turbine configurations. In such situations, the use of the<?pagebreak page2109?> proposed quantitative and comprehensive scan design approach may be beneficial for narrowing down a great deal of arbitrariness and uncertainty associated with campaign planning. Second, LiSBOA offers complete control over the response of the spatial wavelengths of the velocity field for the statistical moments with various orders. This feature is crucial when dealing with turbulent and multiscale flows because it allows the extraction of meaningful information from the flow while filtering out small-scale variability.</p><?xmltex \hack{\clearpage}?>
</sec>

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

<?pagebreak page2110?><app id="App1.Ch1.S1">
  <?xmltex \currentcnt{A}?><label>Appendix A</label><title>List of symbols</title>
      <p id="d1e3821"><table-wrap id="Taba" position="anchor"><oasis:table><oasis:tgroup cols="2">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="left"/>
     <oasis:tbody>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M161" display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M162" display="inline"><mml:mi>y</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M163" display="inline"><mml:mi>z</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Streamwise, spanwise, and vertical</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">Cartesian coordinates</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M164" display="inline"><mml:mi>t</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Time</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M165" display="inline"><mml:mi mathvariant="italic">ρ</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Air density</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M166" display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M167" display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math id="M168" display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Streamwise, spanwise, and vertical</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">velocity components</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M169" display="inline"><mml:mi>L</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Number of realizations and/or scans</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M170" display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Azimuth angle</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M171" display="inline"><mml:mi mathvariant="italic">β</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Elevation angle</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M172" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi mathvariant="italic">θ</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Azimuth angle resolution</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M173" display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">a</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Accumulation time</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M174" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>r</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Gate length</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M175" display="inline"><mml:mrow><mml:msub><mml:mi>N</mml:mi><mml:mi mathvariant="normal">r</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Number of range gates along the laser per beam</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M176" display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Total sampling time</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M177" display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Smoothing parameter</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M178" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Number of iterations</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M179" display="inline"><mml:mrow><mml:msub><mml:mi>R</mml:mi><mml:mtext>max</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Radius of influence</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M180" display="inline"><mml:mrow><mml:mi mathvariant="bold">Δ</mml:mi><mml:mi mathvariant="bold-italic">n</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Half-wavelength vector</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M181" display="inline"><mml:mrow><mml:mi mathvariant="bold">Δ</mml:mi><mml:msub><mml:mi mathvariant="bold-italic">n</mml:mi><mml:mn mathvariant="bold">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Fundamental half-wavelength vector</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M182" display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>d</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Random data spacing</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M183" display="inline"><mml:mrow><mml:mi mathvariant="bold-italic">d</mml:mi><mml:mi mathvariant="bold-italic">x</mml:mi></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Resolution vector in Cartesian coordinates</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M184" display="inline"><mml:mrow><mml:msup><mml:mi>D</mml:mi><mml:mi>m</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Response at the <inline-formula><mml:math id="M185" display="inline"><mml:mi>m</mml:mi></mml:math></inline-formula>th iteration</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M186" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mi mathvariant="normal">I</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Cost function I (data loss)</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M187" display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ϵ</mml:mi><mml:mtext>II</mml:mtext></mml:msup></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Cost function II (standard deviation of</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">the sample mean)</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M188" display="inline"><mml:mi mathvariant="italic">τ</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Integral timescale</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M189" display="inline"><mml:mover accent="true"><mml:mo>.</mml:mo><mml:mo mathvariant="normal" stretchy="false">̃</mml:mo></mml:mover></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Spatial variable in the scaled frame of reference</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M190" display="inline"><mml:mi>D</mml:mi></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Rotor diameter</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M191" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>norm</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min averaged normalized density-corrected</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">hub height wind speed</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M192" display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mtext>norm</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min averaged normalized active power</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M193" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mi mathvariant="normal">∞</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min averaged undisturbed incoming wind speed</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M194" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min averaged hub height wind speed</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M195" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>SD, SCADA</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min based hub height standard deviation</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"/>
         <oasis:entry colname="col2">of wind speed</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M196" display="inline"><mml:mrow><mml:msub><mml:mtext>TI</mml:mtext><mml:mtext>SCADA</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min based hub height turbulence intensity</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M197" display="inline"><mml:mrow><mml:msub><mml:mi>U</mml:mi><mml:mtext>met</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">10 min averaged wind speed from met tower</oasis:entry>
       </oasis:row>
       <oasis:row>
         <oasis:entry colname="col1"><inline-formula><mml:math id="M198" display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mtext>O</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>
         <oasis:entry colname="col2">Obukhov length</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap></p><?xmltex \hack{\clearpage}?>
</app>
  </app-group><notes notes-type="codeavailability"><title>Code availability</title>

      <p id="d1e4462">The LiSBOA algorithm has been implemented in a publicly available code which can be downloaded at <uri>https://github.com/UTD-WindFluX/LiSBOA</uri> (last access: 4 March 2021, <xref ref-type="bibr" rid="bib1.bibx41" id="altparen.56"/>).</p>
  </notes><notes notes-type="authorcontribution"><title>Author contributions</title>

      <p id="d1e4474">SL and GVI developed LiSBOA and prepared the paper. The lidar data were generated as part of a team effort, which included contributions from all three authors. SL implemented LiSBOA in a MATLAB code under the supervision of GVI.</p>
  </notes><notes notes-type="competinginterests"><title>Competing interests</title>

      <p id="d1e4480">The authors declare that they have no conflict of interest.</p>
  </notes><notes notes-type="disclaimer"><title>Disclaimer</title>

      <p id="d1e4486">Any opinions, findings, and conclusions or recommendations expressed in this material are those of the authors and do not necessarily reflect the views of the sponsors.</p>
  </notes><ack><title>Acknowledgements</title><p id="d1e4492">This research has been funded by the National Science Foundation CBET Fluid Dynamics (grant no. 1705837). This material is based upon work supported by the National Science Foundation (grant no. IIP-1362022; Collaborative Research – I/UCRC for Wind Energy, Science, Technology, and Research) and from the WindSTAR I/UCRC Members of Aquanis, Inc., EDP Renewables, Bachmann Electronic Corp., GE Energy, Huntsman, Hexion, Leeward Asset Management, LLC, Pattern Energy, EPRI, LM Wind, Texas Wind Tower, and TPI Composites. The Texas Advanced Computing Center is acknowledged for providing computational resources. The authors acknowledge the support of the owners and operators of the wind farm and the landowners of the test site.</p></ack><notes notes-type="financialsupport"><title>Financial support</title>

      <p id="d1e4497">This research has been supported by the National Science Foundation, Directorate for Engineering (grant nos. 1705837 and IIP-1362022).</p>
  </notes><notes notes-type="reviewstatement"><title>Review statement</title>

      <p id="d1e4503">This paper was edited by Ulla Wandinger and reviewed by two anonymous referees.</p>
  </notes><ref-list>
    <title>References</title>

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    <!--<article-title-html>LiSBOA (LiDAR Statistical Barnes Objective Analysis) for optimal design of lidar scans and retrieval of wind statistics – Part 2: Applications to lidar measurements of wind turbine wakes</article-title-html>
<abstract-html><p>The LiDAR Statistical Barnes Objective Analysis (LiSBOA), presented in Letizia et al. (2021), is a procedure for the optimal design of lidar scans and calculations over a Cartesian grid of the statistical moments of the velocity field. Lidar data collected during a field campaign conducted at a wind farm in complex terrain are analyzed through LiSBOA for two different tests. For both case studies, LiSBOA is leveraged for the optimization of the azimuthal step of the lidar and the retrieval of the mean equivalent velocity and turbulence intensity fields. In the first case, the wake velocity statistics of four utility-scale turbines are reconstructed on a 3D grid, showing LiSBOA's ability to capture complex flow features, such as high-speed jets around the nacelle and the wake turbulent-shear layers. For the second case, the statistics of the wakes generated by four interacting turbines are calculated over a 2D Cartesian grid and compared to the measurements provided by the nacelle-mounted anemometers. Maximum discrepancies, as low as 3&thinsp;% for the mean velocity (with respect to the free stream velocity) and turbulence intensity (in absolute terms), endorse the application of LiSBOA for lidar-based wind resource assessment and diagnostic surveys for wind farms.</p></abstract-html>
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