The airfoil is 43013.  The only other aircraft to use the 43000 family of 
airfoils is the ATR-42/72 air carrier turboprops.

The airfoil is constructed by taking a symmetrical airfoil and bending the

leading edge down at the 15% point to form a 13% camber.  The airfoil 
achieves good low drag performance in cruise as would a symmetrical
airfoil 
and develops good lift coefficients at high angles of attack because of
the 
drooped leading edge.  The airfoil has very little pitching moment which 
lowers the trim drag, further reducing drag.

The bad news is that the airfoil has a big problem with stall recovery and

must only be used in aircraft which are never allowed to stall.  The
problem 
is that once stalled, the wing will not un-stall until a significantly 
greater than stall speed is achieved.  This would be considered
undesirable 
in a trainer or any service where good slow flight behavior is important.

The unpleasant behavior of this series of airfoils worries me when someone

suggests trying to modify and improve the wing with vortex generators and 
wing tip mods.  This is an area to move very slowly in and,  there are
more 
productive ways to improve performance.

The five digit airfoils were very popular with NACA at the time of the 
Ercoupes' development but they are easily improved upon by the six digit 
airfoil series.  When the Ercoupe was reincarnated as the Cherokee series
a 
six digit airfoil was chosen even though the wing could not be constructed

smoothly enough to achieve the benefits of laminar airflow.  The more
common 
of the five digit airfoils are the 23000 series which are very common on 
light twins and some singles although the airfoil shares the poor stall 
behavior of the 43000 series.  When you hear of a light twin loosing
control 
and rolling inverted after the failure of one engine, the airfoil is a big

contributor to the event. 

Is this more than you wanted to know about your wing?

Good luck, 
Bob Condon
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