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diff --git a/_sources/amr-wind/benchmarks.rst.txt b/_sources/amr-wind/benchmarks.rst.txt
@@ -1,14 +1,7 @@
 Benchmark problems using AMR-Wind
 =================================
 
-Atmospheric boundary layer (ABL)
---------------------------------
+.. mdinclude:: ../../amr-wind/atmospheric_boundary_layer/README.md
 
-Convective stability state: stable
-^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
-
-Convective stability state: unstable
-^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
-
-Convective stability state: neutral
-^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
+`Go to cases in repository
+<https://github.com/Exawind/exawind-benchmarks/tree/main/amr-wind/atmospheric_boundary_layer>`__
diff --git a/_sources/exawind/benchmarks.rst.txt b/_sources/exawind/benchmarks.rst.txt
@@ -3,17 +3,10 @@ Benchmark problems using hybrid overset solver (ExaWind)
 
 .. mdinclude:: ../../exawind/NREL_Phase_VI_Turbine/README.md
 
-With RANS
-^^^^^^^^^
+`Go to cases in repository
+<https://github.com/Exawind/exawind-benchmarks/tree/main/exawind/NREL_Phase_VI_Turbine>`__
 
-With RANS and transition model
-^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
+.. mdinclude:: ../../exawind/NREL_5MW_Turbine/README.md
 
-NREL 5-MW turbine
------------------
-
-With rigid blades
-^^^^^^^^^^^^^^^^^
-
-With flexible blades
-^^^^^^^^^^^^^^^^^^^^
+`Go to cases in repository
+<https://github.com/Exawind/exawind-benchmarks/tree/main/exawind/NREL_5MW_Turbine>`__
diff --git a/_sources/nalu-wind/benchmarks.rst.txt b/_sources/nalu-wind/benchmarks.rst.txt
@@ -1,20 +1,17 @@
 Benchmark problems using Nalu-Wind
 ==================================
 
-Two-dimensional (2D) flow past airfoils
----------------------------------------
+.. mdinclude:: ../../nalu-wind/2D_airfoil_Transition/README.md
+
+`Go to cases in repository
+<https://github.com/Exawind/exawind-benchmarks/tree/main/nalu-wind/2D_airfoil_Transition>`__
 
 .. toctree::
-   :maxdepth: 2
+   :maxdepth: 1
 
    clcd_cfd_total
 
-RANS with transition model
-^^^^^^^^^^^^^^^^^^^^^^^^^^
-
-
-Three-dimensional (3D) flow past airfoils
------------------------------------------
+.. mdinclude:: ../../nalu-wind/3D_airfoil_IDDES/README.md
 
-IDDES
-^^^^^
+`Go to cases in repository
+<https://github.com/Exawind/exawind-benchmarks/tree/main/nalu-wind/3D_airfoil_IDDES>`__
diff --git a/_sources/nalu-wind/clcd_cfd_total.ipynb.txt b/_sources/nalu-wind/clcd_cfd_total.ipynb.txt
@@ -4,7 +4,8 @@
    "cell_type": "markdown",
    "metadata": {},
    "source": [
-    "# Coefficients of lift and drag, angle of attack sweep, for DU00-W-212"
+    "# Postprocessing for DU00-W-212: Coefficients of lift and drag\n",
+    "## Angle of attack sweep"
    ]
   },
   {

diff --git a/amr-wind/benchmarks.html b/amr-wind/benchmarks.html
@@ -54,12 +54,7 @@
 </ul>
 <ul class="current">
 <li class="toctree-l1 current"><a class="current reference internal" href="#">Benchmark problems using AMR-Wind</a><ul>
-<li class="toctree-l2"><a class="reference internal" href="#atmospheric-boundary-layer-abl">Atmospheric boundary layer (ABL)</a><ul>
-<li class="toctree-l3"><a class="reference internal" href="#convective-stability-state-stable">Convective stability state: stable</a></li>
-<li class="toctree-l3"><a class="reference internal" href="#convective-stability-state-unstable">Convective stability state: unstable</a></li>
-<li class="toctree-l3"><a class="reference internal" href="#convective-stability-state-neutral">Convective stability state: neutral</a></li>
-</ul>
-</li>
+<li class="toctree-l2"><a class="reference internal" href="#atmospheric-boundary-layer-abl">Atmospheric Boundary Layer (ABL)</a></li>
 </ul>
 </li>
 <li class="toctree-l1"><a class="reference internal" href="published.html">Additional published cases using AMR-Wind</a></li>
@@ -94,17 +89,10 @@
 
   <section id="benchmark-problems-using-amr-wind">
 <h1>Benchmark problems using AMR-Wind<a class="headerlink" href="#benchmark-problems-using-amr-wind" title="Link to this heading"></a></h1>
-<section id="atmospheric-boundary-layer-abl">
-<h2>Atmospheric boundary layer (ABL)<a class="headerlink" href="#atmospheric-boundary-layer-abl" title="Link to this heading"></a></h2>
-<section id="convective-stability-state-stable">
-<h3>Convective stability state: stable<a class="headerlink" href="#convective-stability-state-stable" title="Link to this heading"></a></h3>
-</section>
-<section id="convective-stability-state-unstable">
-<h3>Convective stability state: unstable<a class="headerlink" href="#convective-stability-state-unstable" title="Link to this heading"></a></h3>
-</section>
-<section id="convective-stability-state-neutral">
-<h3>Convective stability state: neutral<a class="headerlink" href="#convective-stability-state-neutral" title="Link to this heading"></a></h3>
-</section>
+<!-- This file is automatically compiled into the website. Begin headings with ## (or lower), not #, to avoid breaking the website heading hierarchy. --><section id="atmospheric-boundary-layer-abl">
+<h2>Atmospheric Boundary Layer (ABL)<a class="headerlink" href="#atmospheric-boundary-layer-abl" title="Link to this heading"></a></h2>
+<p>Add generic description of ABL cases</p>
+<p><a class="reference external" href="https://github.com/Exawind/exawind-benchmarks/tree/main/amr-wind/atmospheric_boundary_layer">Go to cases in repository</a></p>
 </section>
 </section>
 

diff --git a/exawind/benchmarks.html b/exawind/benchmarks.html
@@ -51,16 +51,8 @@
 </ul>
 <ul class="current">
 <li class="toctree-l1 current"><a class="current reference internal" href="#">Benchmark problems using hybrid overset solver (ExaWind)</a><ul>
-<li class="toctree-l2"><a class="reference internal" href="#nrel-phase-vi-turbine">NREL Phase VI Turbine</a><ul>
-<li class="toctree-l3"><a class="reference internal" href="#with-rans">With RANS</a></li>
-<li class="toctree-l3"><a class="reference internal" href="#with-rans-and-transition-model">With RANS and transition model</a></li>
-</ul>
-</li>
-<li class="toctree-l2"><a class="reference internal" href="#nrel-5-mw-turbine">NREL 5-MW turbine</a><ul>
-<li class="toctree-l3"><a class="reference internal" href="#with-rigid-blades">With rigid blades</a></li>
-<li class="toctree-l3"><a class="reference internal" href="#with-flexible-blades">With flexible blades</a></li>
-</ul>
-</li>
+<li class="toctree-l2"><a class="reference internal" href="#nrel-phase-vi-turbine">NREL Phase VI Turbine</a></li>
+<li class="toctree-l2"><a class="reference internal" href="#nrel-5-mw-turbine">NREL 5-MW Turbine</a></li>
 </ul>
 </li>
 </ul>
@@ -109,21 +101,12 @@ <h2>NREL Phase VI Turbine<a class="headerlink" href="#nrel-phase-vi-turbine" tit
 <li><p>Nonlinear twist with blade tip pitch of 3deg</p></li>
 <li><p>Pitch and twist axis at 0.3c</p></li>
 </ul>
-<section id="with-rans">
-<h3>With RANS<a class="headerlink" href="#with-rans" title="Link to this heading"></a></h3>
-</section>
-<section id="with-rans-and-transition-model">
-<h3>With RANS and transition model<a class="headerlink" href="#with-rans-and-transition-model" title="Link to this heading"></a></h3>
-</section>
-</section>
+<p><a class="reference external" href="https://github.com/Exawind/exawind-benchmarks/tree/main/exawind/NREL_Phase_VI_Turbine">Go to cases in repository</a></p>
+<!-- This file is automatically compiled into the website. Begin headings with ## (or lower), not #, to avoid breaking the website heading hierarchy. --></section>
 <section id="nrel-5-mw-turbine">
-<h2>NREL 5-MW turbine<a class="headerlink" href="#nrel-5-mw-turbine" title="Link to this heading"></a></h2>
-<section id="with-rigid-blades">
-<h3>With rigid blades<a class="headerlink" href="#with-rigid-blades" title="Link to this heading"></a></h3>
-</section>
-<section id="with-flexible-blades">
-<h3>With flexible blades<a class="headerlink" href="#with-flexible-blades" title="Link to this heading"></a></h3>
-</section>
+<h2>NREL 5-MW Turbine<a class="headerlink" href="#nrel-5-mw-turbine" title="Link to this heading"></a></h2>
+<p>Add generic description of NREL 5-MW Turbine cases</p>
+<p><a class="reference external" href="https://github.com/Exawind/exawind-benchmarks/tree/main/exawind/NREL_5MW_Turbine">Go to cases in repository</a></p>
 </section>
 </section>
 

diff --git a/index.html b/index.html
@@ -101,7 +101,7 @@ <h2>ExaWind<a class="headerlink" href="#exawind" title="Link to this heading">
 <ul>
 <li class="toctree-l1"><a class="reference internal" href="exawind/benchmarks.html">Benchmark problems using hybrid overset solver (ExaWind)</a><ul>
 <li class="toctree-l2"><a class="reference internal" href="exawind/benchmarks.html#nrel-phase-vi-turbine">NREL Phase VI Turbine</a></li>
-<li class="toctree-l2"><a class="reference internal" href="exawind/benchmarks.html#nrel-5-mw-turbine">NREL 5-MW turbine</a></li>
+<li class="toctree-l2"><a class="reference internal" href="exawind/benchmarks.html#nrel-5-mw-turbine">NREL 5-MW Turbine</a></li>
 </ul>
 </li>
 </ul>
@@ -112,7 +112,7 @@ <h2>AMR-Wind<a class="headerlink" href="#amr-wind" title="Link to this heading">
 <div class="toctree-wrapper compound">
 <ul>
 <li class="toctree-l1"><a class="reference internal" href="amr-wind/benchmarks.html">Benchmark problems using AMR-Wind</a><ul>
-<li class="toctree-l2"><a class="reference internal" href="amr-wind/benchmarks.html#atmospheric-boundary-layer-abl">Atmospheric boundary layer (ABL)</a></li>
+<li class="toctree-l2"><a class="reference internal" href="amr-wind/benchmarks.html#atmospheric-boundary-layer-abl">Atmospheric Boundary Layer (ABL)</a></li>
 </ul>
 </li>
 <li class="toctree-l1"><a class="reference internal" href="amr-wind/published.html">Additional published cases using AMR-Wind</a></li>

diff --git a/nalu-wind/benchmarks.html b/nalu-wind/benchmarks.html
@@ -23,7 +23,7 @@
     <script src="../_static/js/theme.js"></script>
     <link rel="index" title="Index" href="../genindex.html" />
     <link rel="search" title="Search" href="../search.html" />
-    <link rel="next" title="Coefficients of lift and drag, angle of attack sweep, for DU00-W-212" href="clcd_cfd_total.html" />
+    <link rel="next" title="Postprocessing for DU00-W-212: Coefficients of lift and drag" href="clcd_cfd_total.html" />
     <link rel="prev" title="Additional published cases using AMR-Wind" href="../amr-wind/published.html" /> 
 </head>
 
@@ -59,14 +59,10 @@
 <ul class="current">
 <li class="toctree-l1 current"><a class="current reference internal" href="#">Benchmark problems using Nalu-Wind</a><ul>
 <li class="toctree-l2"><a class="reference internal" href="#two-dimensional-2d-flow-past-airfoils">Two-dimensional (2D) flow past airfoils</a><ul>
-<li class="toctree-l3"><a class="reference internal" href="clcd_cfd_total.html">Coefficients of lift and drag, angle of attack sweep, for DU00-W-212</a></li>
-<li class="toctree-l3"><a class="reference internal" href="#rans-with-transition-model">RANS with transition model</a></li>
-</ul>
-</li>
-<li class="toctree-l2"><a class="reference internal" href="#three-dimensional-3d-flow-past-airfoils">Three-dimensional (3D) flow past airfoils</a><ul>
-<li class="toctree-l3"><a class="reference internal" href="#iddes">IDDES</a></li>
+<li class="toctree-l3"><a class="reference internal" href="clcd_cfd_total.html">Postprocessing for DU00-W-212: Coefficients of lift and drag</a></li>
 </ul>
 </li>
+<li class="toctree-l2"><a class="reference internal" href="#three-dimensional-3d-flow-past-airfoils">Three-dimensional (3D) flow past airfoils</a></li>
 </ul>
 </li>
 </ul>
@@ -97,22 +93,27 @@
 
   <section id="benchmark-problems-using-nalu-wind">
 <h1>Benchmark problems using Nalu-Wind<a class="headerlink" href="#benchmark-problems-using-nalu-wind" title="Link to this heading"></a></h1>
-<section id="two-dimensional-2d-flow-past-airfoils">
+<!-- This file is automatically compiled into the website. Begin headings with ## (or lower), not #, to avoid breaking the website heading hierarchy. --><section id="two-dimensional-2d-flow-past-airfoils">
 <h2>Two-dimensional (2D) flow past airfoils<a class="headerlink" href="#two-dimensional-2d-flow-past-airfoils" title="Link to this heading"></a></h2>
+<p>These benchmark cases employ a RANS modeling framework and serve as validation and verification of the 1-eq Gamma Transition Model.
+They include the following airfoils and flow parameters:</p>
+<ul class="simple">
+<li><p>NASA NLF(1)-0416 airfoil at M=0.1, Re=4M, Tu=0.15%</p></li>
+<li><p>TU Delft DU00-W-212 airfoil at M=0.1, Re=3M, Tu=0.0864%</p></li>
+</ul>
+<p><a class="reference external" href="https://github.com/Exawind/exawind-benchmarks/tree/main/nalu-wind/2D_airfoil_Transition">Go to cases in repository</a></p>
 <div class="toctree-wrapper compound">
 <ul>
-<li class="toctree-l1"><a class="reference internal" href="clcd_cfd_total.html">Coefficients of lift and drag, angle of attack sweep, for DU00-W-212</a></li>
+<li class="toctree-l1"><a class="reference internal" href="clcd_cfd_total.html">Postprocessing for DU00-W-212: Coefficients of lift and drag</a></li>
 </ul>
 </div>
-<section id="rans-with-transition-model">
-<h3>RANS with transition model<a class="headerlink" href="#rans-with-transition-model" title="Link to this heading"></a></h3>
-</section>
-</section>
+<!-- This file is automatically compiled into the website. Begin headings with ## (or lower), not #, to avoid breaking the website heading hierarchy. --></section>
 <section id="three-dimensional-3d-flow-past-airfoils">
 <h2>Three-dimensional (3D) flow past airfoils<a class="headerlink" href="#three-dimensional-3d-flow-past-airfoils" title="Link to this heading"></a></h2>
-<section id="iddes">
-<h3>IDDES<a class="headerlink" href="#iddes" title="Link to this heading"></a></h3>
-</section>
+<p>These benchmark cases use IDDES for turbulence modeling, and they simulate flow past a NACA 0021 airfoil.</p>
+<p>Publication:
+Bidadi, S.; Vijayakumar, G.; Deskos, G.; Sprague, M. Three-Dimensional Aerodynamics and Vortex-Shedding Characteristics of Wind Turbine Airfoils over 360-Degree Angles of Attack. Energies 2024, 17, 4328. <a class="reference external" href="https://doi.org/10.3390/en17174328">https://doi.org/10.3390/en17174328</a></p>
+<p><a class="reference external" href="https://github.com/Exawind/exawind-benchmarks/tree/main/nalu-wind/3D_airfoil_IDDES">Go to cases in repository</a></p>
 </section>
 </section>
 
@@ -121,7 +122,7 @@ <h3>IDDES<a class="headerlink" href="#iddes" title="Link to this heading"></a
           </div>
           <footer><div class="rst-footer-buttons" role="navigation" aria-label="Footer">
         <a href="../amr-wind/published.html" class="btn btn-neutral float-left" title="Additional published cases using AMR-Wind" accesskey="p" rel="prev"><span class="fa fa-arrow-circle-left" aria-hidden="true"></span> Previous</a>
-        <a href="clcd_cfd_total.html" class="btn btn-neutral float-right" title="Coefficients of lift and drag, angle of attack sweep, for DU00-W-212" accesskey="n" rel="next">Next <span class="fa fa-arrow-circle-right" aria-hidden="true"></span></a>
+        <a href="clcd_cfd_total.html" class="btn btn-neutral float-right" title="Postprocessing for DU00-W-212: Coefficients of lift and drag" accesskey="n" rel="next">Next <span class="fa fa-arrow-circle-right" aria-hidden="true"></span></a>
     </div>
 
   <hr/>

diff --git a/nalu-wind/clcd_cfd_total.html b/nalu-wind/clcd_cfd_total.html
@@ -6,7 +6,7 @@
   <meta charset="utf-8" /><meta name="viewport" content="width=device-width, initial-scale=1" />
 
   <meta name="viewport" content="width=device-width, initial-scale=1.0" />
-  <title>Coefficients of lift and drag, angle of attack sweep, for DU00-W-212 &mdash; ExaWind Benchmarks 0.1 documentation</title>
+  <title>Postprocessing for DU00-W-212: Coefficients of lift and drag &mdash; ExaWind Benchmarks 0.1 documentation</title>
       <link rel="stylesheet" type="text/css" href="../_static/pygments.css?v=fa44fd50" />
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       <link rel="stylesheet" type="text/css" href="../_static/copybutton.css?v=76b2166b" />
@@ -58,8 +58,10 @@
 <ul class="current">
 <li class="toctree-l1 current"><a class="reference internal" href="benchmarks.html">Benchmark problems using Nalu-Wind</a><ul class="current">
 <li class="toctree-l2 current"><a class="reference internal" href="benchmarks.html#two-dimensional-2d-flow-past-airfoils">Two-dimensional (2D) flow past airfoils</a><ul class="current">
-<li class="toctree-l3 current"><a class="current reference internal" href="#">Coefficients of lift and drag, angle of attack sweep, for DU00-W-212</a></li>
-<li class="toctree-l3"><a class="reference internal" href="benchmarks.html#rans-with-transition-model">RANS with transition model</a></li>
+<li class="toctree-l3 current"><a class="current reference internal" href="#">Postprocessing for DU00-W-212: Coefficients of lift and drag</a><ul>
+<li class="toctree-l4"><a class="reference internal" href="#angle-of-attack-sweep">Angle of attack sweep</a></li>
+</ul>
+</li>
 </ul>
 </li>
 <li class="toctree-l2"><a class="reference internal" href="benchmarks.html#three-dimensional-3d-flow-past-airfoils">Three-dimensional (3D) flow past airfoils</a></li>
@@ -82,7 +84,7 @@
   <ul class="wy-breadcrumbs">
       <li><a href="../index.html" class="icon icon-home" aria-label="Home"></a></li>
           <li class="breadcrumb-item"><a href="benchmarks.html">Benchmark problems using Nalu-Wind</a></li>
-      <li class="breadcrumb-item active">Coefficients of lift and drag, angle of attack sweep, for DU00-W-212</li>
+      <li class="breadcrumb-item active">Postprocessing for DU00-W-212: Coefficients of lift and drag</li>
       <li class="wy-breadcrumbs-aside">
             <a href="../_sources/nalu-wind/clcd_cfd_total.ipynb.txt" rel="nofollow"> View page source</a>
       </li>
@@ -92,8 +94,10 @@
           <div role="main" class="document" itemscope="itemscope" itemtype="http://schema.org/Article">
            <div itemprop="articleBody">
 
-  <section id="coefficients-of-lift-and-drag-angle-of-attack-sweep-for-du00-w-212">
-<h1>Coefficients of lift and drag, angle of attack sweep, for DU00-W-212<a class="headerlink" href="#coefficients-of-lift-and-drag-angle-of-attack-sweep-for-du00-w-212" title="Link to this heading"></a></h1>
+  <section id="postprocessing-for-du00-w-212-coefficients-of-lift-and-drag">
+<h1>Postprocessing for DU00-W-212: Coefficients of lift and drag<a class="headerlink" href="#postprocessing-for-du00-w-212-coefficients-of-lift-and-drag" title="Link to this heading"></a></h1>
+<section id="angle-of-attack-sweep">
+<h2>Angle of attack sweep<a class="headerlink" href="#angle-of-attack-sweep" title="Link to this heading"></a></h2>
 <div class="cell docutils container">
 <div class="cell_input docutils container">
 <div class="highlight-ipython3 notranslate"><div class="highlight"><pre><span></span><span class="kn">import</span> <span class="nn">yaml</span>
@@ -190,6 +194,7 @@ <h1>Coefficients of lift and drag, angle of attack sweep, for DU00-W-212<a class
 <img alt="../_images/6cc6e300fbc76a168c08ee09350f6bb84ae7ba8bd6003b4f48b9ebcdd4bf0cf2.png" src="../_images/6cc6e300fbc76a168c08ee09350f6bb84ae7ba8bd6003b4f48b9ebcdd4bf0cf2.png" />
 </div>
 </div>
+</section>
 </section>
 
 

diff --git a/objects.inv b/objects.inv