dragonfly_sim.utils.postprocessor_utils
=======================================

.. py:module:: dragonfly_sim.utils.postprocessor_utils


Functions
---------

.. autoapisummary::

   dragonfly_sim.utils.postprocessor_utils.cross_2D
   dragonfly_sim.utils.postprocessor_utils.moment_integrand


Module Contents
---------------

.. py:function:: cross_2D(x, y)

.. py:function:: moment_integrand(force_vec, lever_vec, dimensions)

   
   The pitching-moment integrand: the component of (lever x force) about the
   axis the aerofoil/wing pitches around.

   This exists because cross_2D above is a genuinely 2D expression --
   x[0]*y[1] - x[1]*y[0] reads only components 0 and 1 -- so applying it
   unchanged to 3D vectors silently returns the moment about the VERTICAL
   axis (a yawing moment) rather than the pitching moment. The two coordinate
   conventions in use here disagree about which index is "vertical":

     2D: x = chordwise, y = vertical
         -> the pitch axis is z, and cross_2D(force, lever) is that
            component (up to the sign convention baked into compute_cm).
     3D: x = chordwise, y = spanwise, z = vertical
         (see the mesh note at the top of wing_opt.py)
         -> the pitch axis is y, i.e. (lever x force)_y = r_z*F_x - r_x*F_z.

   The 2D branch returns exactly the previous expression, so 2D results are
   unchanged bit-for-bit.















   ..
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