Gallery
=======

Click on any image to zoom. Press the "back" button to return to the gallery.

.. list-table::
   :widths: 50 50
   :class: only-dark

   * - .. figure:: images/pymead_main_screenshot_dark.*
          :width: 100%
          :class: only-dark

          Aero-propulsive analysis of an optimized multi-element airfoil

     - .. figure:: images/xfoil_opt_10x_dark.*
          :width: 100%
          :class: only-dark

          Optimization using XFOIL (10x speed)

   * - .. figure:: images/n0012_analysis_xfoil_dark.*
          :width: 100%
          :class: only-dark

          XFOIL analysis of the NACA 0012 airfoil at :math:`M=0.1` and :math:`\alpha=\{0^\circ,1^\circ,2^\circ\}`

     - .. figure:: images/sc20612_analysis_dark.*
          :width: 100%
          :class: only-dark

          MSES analysis of the NASA SC20612 airfoil at :math:`M=0.67` and :math:`\alpha=\{0^\circ,1^\circ\}`

   * - .. figure:: images/desvar_mod_dark.*
          :width: 100%
          :class: only-dark

          Modification of design variables

     - .. figure:: images/field_plotting_dark.*
          :width: 100%
          :class: only-dark

          Plotting aerodynamic field variables

   * - .. figure:: images/polar_analysis_dark.*
          :width: 100%
          :class: only-dark

          Polar analysis workflow for a custom airfoil

     - .. figure:: images/polars_dark.*
          :width: 100%
          :class: only-dark

          Aerodynamic polars for a custom airfoil

   * - .. figure:: images/sc20612_matching_4x_speed_dark.*
          :width: 100%
          :class: only-dark

          Matching a NASA SC20612 airfoil with Bézier curves (4x speed)

     - .. figure:: user/images/gui_customize_dark.*
          :width: 100%
          :class: only-dark

          Customization of the GUI


.. list-table::
   :widths: 50 50
   :class: only-light

   * - .. figure:: images/pymead_main_screenshot_light.*
          :width: 100%
          :class: only-light

          Aero-propulsive analysis of an optimized multi-element airfoil

     - .. figure:: images/xfoil_opt_10x_light.*
          :width: 100%
          :class: only-light

          Optimization using XFOIL (10x speed)

   * - .. figure:: images/n0012_analysis_xfoil_light.*
          :width: 100%
          :class: only-light

          XFOIL analysis of the NACA 0012 airfoil at :math:`M=0.1` and :math:`\alpha=\{0^\circ,1^\circ,2^\circ\}`

     - .. figure:: images/sc20612_analysis_light.*
          :width: 100%
          :class: only-light

          MSES analysis of the NASA SC20612 airfoil at :math:`M=0.67` and :math:`\alpha=\{0^\circ,1^\circ\}`

   * - .. figure:: images/desvar_mod_light.*
          :width: 100%
          :class: only-light

          Modification of design variables

     - .. figure:: images/field_plotting_light.*
          :width: 100%
          :class: only-light

          Plotting aerodynamic field variables

   * - .. figure:: images/polar_analysis_light.*
          :width: 100%
          :class: only-light

          Polar analysis workflow for a custom airfoil

     - .. figure:: images/polars_light.*
          :width: 100%
          :class: only-light

          Aerodynamic polars for a custom airfoil

   * - .. figure:: images/sc20612_matching_4x_speed_light.*
          :width: 100%
          :class: only-light

          Matching a NASA SC20612 airfoil with Bézier curves (4x speed)

     - .. figure:: user/images/gui_customize_light.*
          :width: 100%
          :class: only-light

          Customization of the GUI