:orphan:

.. ****************************************************************************
.. CUI//REL TO USA ONLY
..
.. The Advanced Framework for Simulation, Integration, and Modeling (AFSIM)
..
.. The use, dissemination or disclosure of data in this file is subject to
.. limitation or restriction. See accompanying README and LICENSE for details.
.. ****************************************************************************

Mover Creator Standard Airfoil Templates
++++++++++++++++++++++++++++++++++++++++

Mover Creator provides a set of predefined standard airfoil templates that can be used for any :ref:`Surfaces` (fixed or controlled) defined in the :doc:`Geometry<mc_geometry>` page.

.. table::
   :align: left

   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/bac-3xx.png      | **BAC 300 series**                                   |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`E-HJ-41A-1<E-HJ-41A-1>`                        |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 9% at 40% chord                               |
   |                                    |    * - max camber                                    |
   |                                    |      - 1.8% at 30% chord                             |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 12.0 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -8.0 deg                                      |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.20                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -0.51                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.185                                         |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.01065                                       |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.02814                                      |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/bac-4xx.png      | **BAC 400 series**                                   |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`P-MJ-21A-1<P-MJ-21A-1>`                        |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 12.5% at 29.7% chord                          |
   |                                    |    * - max camber                                    |
   |                                    |      - 0.8% at 10% chord                             |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      -  15.75 deg                                    |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -15.75 deg                                    |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      -  1.56                                         |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -1.287                                        |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.130                                         |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0063                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.0088                                       |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-0008.png    | **NACA 0008**                                        |
   |                                    |                                                      |
   |                                    | Not currently used in any vehicle template           |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 8% at 30% chord                               |
   |                                    |    * - max camber                                    |
   |                                    |      - 0% at 0% chord                                |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 11.5 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -11.5 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      -  1.1                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      -  -1.1                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.004                                         |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-0012.png    | **NACA 0012**                                        |
   |                                    |                                                      |
   |                                    | Used for fins on all                                 |
   |                                    | :ref:`Weapon<Weapons>` templates                     |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 12% at 30% chord                              |
   |                                    |    * - max camber                                    |
   |                                    |      - 0% at 0% chord                                |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 15.5 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -15.5 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.37                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -1.37                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0053                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-6716.png    | **NACA 6716**                                        |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`A-M4-22A-1<A-M4-22A-1>`                        |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 16% at 30% chord                              |
   |                                    |    * - max camber                                    |
   |                                    |      - 6% at 70% chord                               |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 19.0 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -15.0 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.83                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -0.61                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.906                                         |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0075                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.254                                        |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-63409.png   | **NACA 63A409**                                      |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`R-MJ-11A-1<R-MJ-11A-1>`                        |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 8.7% at 35.5% chord                           |
   |                                    |    * - max camber                                    |
   |                                    |      - 2.8% at 52.5% chord                           |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 13.0 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -9 deg                                        |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      -  1.365                                        |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -0.442                                        |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.365                                         |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0047                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.0825                                       |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-64012.png   | **NACA 64(1)-012**                                   |
   |                                    |                                                      |
   |                                    | Used for all non-wing surfaces for                   |
   |                                    | :ref:`Aircraft` templates                            |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 12% at 40% chord                              |
   |                                    |    * - max camber                                    |
   |                                    |      - 0% at 0% chord                                |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 13.0 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -13.0 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.15                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -1.15                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0054                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-64206.png   | **NACA 64-206**                                      |
   |                                    |                                                      |
   |                                    | Used for the wings of all                            |
   |                                    | :ref:`Fighter` and :ref:`Drone` templates            |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 6% at 40% chord                               |
   |                                    |    * - max camber                                    |
   |                                    |      - 1.1% at 50% chord                             |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 7.75 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -7.75 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 0.8275                                        |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -0.527                                        |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.145                                         |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0037                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.042                                        |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-633218.png  | **NACA 63(3)-218**                                   |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`B-H3-81A-1<B-H3-81A-1>` template               |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 18% at 34% chord                              |
   |                                    |    * - max camber                                    |
   |                                    |      - 1.1% at 25% chord                             |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 19.0 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -18.5 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.35                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -1.16                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.15                                          |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0074                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.0346                                       |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/naca-653018.png  | **NACA 65(3)-018**                                   |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`B-H1-80W-1<B-H1-80W-1>` and                    |
   |                                    | :ref:`B-H4-40W-1<B-H4-40W-1>` templates              |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 18% at 40% chord                              |
   |                                    |    * - max camber                                    |
   |                                    |      - 0% at 0% chord                                |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 18.0 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -18.0 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.14                                          |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -1.14                                         |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.0068                                        |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - 0.0                                           |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   | .. image:: images/nasa-20412.png   | **NASA SC(2)-0412**                                  |
   |                                    |                                                      |
   |                                    | Used for the wing of the                             |
   |                                    | :ref:`K-MJ-21A-1<K-MJ-21A-1>` and                    |
   |                                    | :ref:`C-HJ-41A-1<C-HJ-41A-1>` templates              |
   |                                    |                                                      |
   |                                    | .. list-table::                                      |
   |                                    |    :align: left                                      |
   |                                    |    :widths: 35 65                                    |
   |                                    |                                                      |
   |                                    |    * - max thickness                                 |
   |                                    |      - 12% at 37% chord                              |
   |                                    |    * - max camber                                    |
   |                                    |      - 1.3% at 83% chord                             |
   |                                    |    * - :math:`\alpha_{C_{L_{max}}}`                  |
   |                                    |      - 15.5 deg                                      |
   |                                    |    * - :math:`\alpha_{C_{L_{min}}}`                  |
   |                                    |      - -16.5 deg                                     |
   |                                    |    * - :math:`C_{L_{max}}`                           |
   |                                    |      - 1.6412                                        |
   |                                    |    * - :math:`C_{L_{min}}`                           |
   |                                    |      - -1.3565                                       |
   |                                    |    * - :math:`C_{L_0}`                               |
   |                                    |      - 0.255                                         |
   |                                    |    * - :math:`C_{d_0}`                               |
   |                                    |      - 0.006                                         |
   |                                    |    * - :math:`C_{m_0}`                               |
   |                                    |      - -0.08                                         |
   |                                    |                                                      |
   |                                    | |                                                    |
   |                                    |                                                      |
   +------------------------------------+------------------------------------------------------+