I'm not aware of this feature of compufoil, but I only
have the basic version.

The angle of attack (AOA) of a wing is its angle to
the freestream.  If you want your fuz to line up
parallel with the freestream (and you probably do)
while the wing is at x degrees to the freestream then
set the wing at x degrees to the fuz. 

Good luck.  Anyone who bags a wing has earned it.

Jeb.

P.S.  I'm an amateur. Any aerodynamic advice or
comment by me may be hazardous or, even worse, wrong.


--- Steve Gwilliam <[EMAIL PROTECTED]> wrote:
> I am building a slope plane.  I have made the wing
> using vacuum bagging.  I
> am using the RG15 airfoil as generated by compufoil.
>  The information
> provided by compufoil tells me that the ideal angle
> of attack is .23 degrees
> or almost flat.  Is this angle relative to the level
> line of the fuselage
> that the wing will be resting on, or am I way off on
> that assumption?  
> Any information on how to seat the wing at the
> proper angle would much
> appreciated.
> 
> Thanks 
> 


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