Docs @ 52e8af1

Author: MFC Action

documentation/architecture.html

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 <td class="markdownTableBodyNone"><span class="tt">m_chemistry</span>  </td><td class="markdownTableBodyNone">Multi-species chemistry interface for thermodynamic properties, reaction rates, and transport coefficients  </td></tr>
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-<td class="markdownTableBodyNone"><span class="tt">m_acoustic_src</span>  </td><td class="markdownTableBodyNone">Applies acoustic pressure source terms including focused, planar, and broadband transducers  </td></tr>
+<td class="markdownTableBodyNone"><span class="tt">m_acoustic_src</span>  </td><td class="markdownTableBodyNone">One-way acoustic source injection, Maeda and Colonius JCP (2017)  </td></tr>
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 <td class="markdownTableBodyNone"><span class="tt">m_body_forces</span>  </td><td class="markdownTableBodyNone">Computes gravitational and user-defined body force source terms for the momentum equations  </td></tr>
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 <li><b>Add the module to <span class="tt">docs/module_categories.json</span></b> so it appears in this page</li>
 </ol>
 <p>Follow the pattern of existing modules like <span class="tt">m_body_forces</span> (simple) or <span class="tt">m_viscous</span> (more involved) as a template.</p>
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documentation/case.html

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 <li><span class="tt">length_x[y,z]</span> is the length of the patch in the x[y,z]-direction.</li>
 <li><span class="tt">radius</span> is the radius to be used for circular patches.</li>
 <li><span class="tt">theta</span> allows for the angle of attach of airfoil patches to be changed.</li>
-<li><span class="tt">c</span>, <span class="tt">t</span>, <span class="tt">p</span>, and <span class="tt">m</span> specify the parameters for a NACA airfoil. <span class="tt">m</span> is the maximum camber, <span class="tt">p</span> is the location of maximum camber, <span class="tt">c</span> is the coord length, and <span class="tt">t</span> is the thickness. Additional details on this specification can be found in <a href="https://web.stanford.edu/~cantwell/AA200_Course_Material/The%20NACA%20airfoil%20series.pdf">The Naca Airfoil Series</a></li>
+<li><span class="tt">c</span>, <span class="tt">t</span>, <span class="tt">p</span>, and <span class="tt">m</span> specify the parameters for a NACA airfoil. <span class="tt">m</span> is the maximum camber, <span class="tt">p</span> is the location of maximum camber, <span class="tt">c</span> is the coord length, and <span class="tt">t</span> is the thickness. Additional details on this specification can be found in <a href="https://en.wikipedia.org/wiki/NACA_airfoil">NACA airfoil</a>.</li>
 <li><span class="tt">slip</span> applies a slip boundary to the surface of the patch if true and a no-slip boundary condition to the surface if false.</li>
 <li>Please see <a class="el" href="#sec-patches" title="3. Patches">Patch Parameters</a> for the descriptions of <span class="tt">model_filepath</span>, <span class="tt">model_scale</span>, <span class="tt">model_rotate</span>, <span class="tt">model_translate</span>, <span class="tt">model_spc</span>, and <span class="tt">model_threshold</span>.</li>
 <li><span class="tt">moving_ibm</span> sets the method by which movement will be applied to the immersed boundary. Using 0 will result in no movement. Using 1 will result 1-way coupling where the boundary moves at a constant rate and applied forces to the fluid based upon it's own motion. In 1-way coupling, the fluid does not apply forces back onto the IB. Using 2 will result in 2-way coupling, where the boundary pushes on the fluid and the fluid pushes back on the boundary via pressure and viscous forces. If external forces are applied, the boundary will also experience those forces.</li>

documentation/case_constraints.html

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 <p>💡 <b>Tip:</b> If you encounter a validation error, check the relevant section above or review <a href="https://github.com/MFlowCode/MFC/blob/master/toolchain/mfc/case_validator.py"><span class="tt">case_validator.py</span></a> for complete validation logic.</p>
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documentation/cli-reference.html

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 Debug Logging (<span class="tt">-d, --debug-log</span>)</h3>
 <p>Enables debug logging for the Python toolchain (mfc.sh internals). This is for troubleshooting the build system, not the MFC simulation code.</p>
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documentation/examples.html

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 Final Condition (Density)</h3>
 <p><img src="final-2D_forward_facing_step-example.png" alt="" class="inline"/></p>
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documentation/parameters.html

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 <div class="line"> </div>
 <div class="line"># Filter by type</div>
 <div class="line">./mfc.sh params -t real weno</div>
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documentation/physics_constraints.html

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 <li>FFT WRT incompatible with cylindrical coordinates</li>
 <li>FFT WRT requires global dimensions divisible by 2</li>
 </ul>
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