Ameet:

 Thanks for setting me straight on the terminology.  What I used for wing
area is exactly what you sdescribe as I used  36 inches x 94 inches  for
the outbboard wings on mine to run through the theoretical stall speed
calcs to arrive at max allowable gross for the 51 mph stallof 887#  for my
bird.

I am depending on engine & Prop choice as well as the drag of the Tri-gear
to get the speed under the 138 mph limit.  I would of course love the
"Pocket Rocket" status afforded by some of the larger engine sizes.

Don

Ameet Savant wrote:

> Eric - The airfoil and hence the curvature neither the
> thickness of it has any bearing on the wing area for
> aerodynamic calculations. In other words, simply
> calculate the area of the polygon traced by the wing
> to get the wing area.
>
> Don - MAC is a weighted average of all cord lengths on
> a semi-span. This is useful for simplifing aerodynamic
> calculations on a tapered wing. MAC is same as chord
> on a rectangular wing.
>
> Ameet Savant
> Omaha, NE
>
> --- D F Lively <[email protected]> wrote:
>
> > Eric:
> >
> > I can be wrong on this but I think that is whaht is
> > ment by the MACwhich is the
> > lingthof the line 1l2 way between the upper and
> > lower surface which would be
> > slightly longer.  I would not worry about the
> > theoretical benifits of that
> > though because as a practical mater there are
> > probably enough imperfections
> > elsewhere to eat up what little is gained by
> > cosidering the difference.
> >
> > Don
> >
> >
> ----------------------------------------------------------------
> >
> > Eric Anderson wrote:
> >
> > > I read somewhere that the square footage of a wing
> > is what you would get if
> > > if you stripped the upper surface off and laid it
> > out flat. So it is always
> > > a little more than the chord x span.
> > >
> > > -Eric in Mpls
>
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