The Davis Akro Pro hybrid wing. This wing was designed to
      incorporate the best of both types of construction  (foam and built
      up). There are advantages of both methods of construction that I liked so
      I decided to construct a wing combining all of the good ones. 
      Built up wing advantages are lightness and the scale look of ribs
      (depends on airplane).  Foam wing advantages are mainly accuracy and
      speed of construction.
      Once the core airfoil was cut I cut the tube hole and epoxied the tube
      in place. After the tube was in place I cut a slot in the foam down to the
      tube on the top and bottom to place the 1/4 inch end grain balsa. The
      balsa was placed end grain to keep it from crushing and was capped with a
      molded in carbon spar that sat flush with the foam core.  A trough
      was cut to accept the carbon tow and epoxy that extended from the root to
      the tip. The carbon tow was gradually decreased in cross section towards
      the tip, this was done to avoid a stress riser and to save weight. End grain balsa was also
      added to the core where the aileron control arm would locate. (The
      carbon spar and end grain tube caps cannot be seen since they are buried
      in the foam but there is a rough drawing of the wing tube, end grain and
      carbon spar below. This wing was built before this web site was even thought of
      so this article is in retrospect).
      The grooves for the ribs were cut with a modified soldering iron tip
      with a depth gauge attached. The wood strip ribs were added to the grooves
      and glued to the spar after which they were sanded flush with the top
      surface of the foam. This is where the real savings in time takes place
      since the ribs do not have to be plotted or cut out. By placing the strip
      ribs in the foam grooves you could literally place the ribs at any angle,
      warren truss or geodetic construction could result effortlessly. If you
      were building a wing where you didn't want any foam left you could run the
      strip ribs between the leading edge and trailing edges with carbon fiber
      reinforcements as a spar. Once you start thinking outside of the box many
      options become available.  The wood leading edge was glued to the leading edge
      of the foam wing and shaped to match the contour of the airfoil.
      The next step was to vacuum the sheeting that you see on the wing down
      to the foam using epoxy as the adhesive. The sheeting overlapped the strip
      ribs about 1/4 inch and completely overlapped the leading edge. By placing
      the sheeting over the leading edge you gain some strength and hide a seam.
      At this point when the wing is bagged there is still foam between the
      false ribs. Once the wing was cured and taken out of the bag  the
      foam was removed from between the strip ribs and the vertical grain
      supports are added between the top and bottom strip ribs. The rib caps are
      added at this time to match the sheeting.
      The back portion of the wing is cut away so that a full depth and full
      span trailing edge (which goes in front of the aileron) could be added to
      the wing. At this time the aileron was capped with a leading edge and
      trailing edge along with the end caps.  I wanted the trailing edge of
      the wing that was in front of the aileron to extend the full span to get
      away from a stress riser at the root of the aileron cutout on the wing.
      The trailing edge of the wing at the root was also glued back on the wing
      at this step.
      For extra lightness the leading edge could be cored out after
      bagging.  All coring has to be done after the bagging process since
      the cored wing will not hold up under any vacuum, tried that to see what
      would happen, won't mention the results here.