Hi Gang

I down loaded the profilli software as suggested by steve J - brilliant - I 
will send the owner the $10 or whatever to get the full version.

I figured steve was talking through his neck - P51 wing sectrion - oh yeah - 
well I the P51 section is there and I did the comparrison he reccomended - 
P51 against the AS 5046 - amazing similarity.

Then came the discussion from the airfoil boffs about the cusp (tuck???).  
Take the cusp out of a 4046 and you have a P51 root section -  I will do it 
like that.

Ron







> > > I am interested in the strange "tuck" underneath the trailing
> > > edge - the last few mm seem to droop down leaving a
> > > concave area right at the back (underneath).
>
>That trailing edge cusp does several different things.  When comparing to a
>related airfoil without the cusp, the coefficient of lift will be higher at
>a given angle of attack, the pitch moment will be more negative, and the
>boundary layer separation will tend to stay closer to the trailing
>edge.  The maximum coefficient of lift of the two different airfoils will
>be approximately the same, but the cusped airfoil will reach it at a lower
>angle of attack.  All of these parameters are compromises that affect the
>overall design of the airplane.
>
>It can be an acceptable airfoil for a wing root but will be a poor choice
>for a control surface.  Aileron control forces will be high.  It is a less
>than optimum choice for an airfoil that is intended to be laminar over a
>wide range angle of attack.
>
>
>Don Reid  -  donreid "at" erols.com
>Bumpass, Va
>
>Visit my web sites at:
>
>AeroFoil, a 2-D Airfoil Design And Analysis Computer Program:
>http://www.eaa231.org/AeroFoil/index.htm
>
>KR2XL construction: http://users.erols.com/donreid/kr_page.htm
>Aviation Surplus: http://users.erols.com/donreid/Airparts.htm
>EAA Chapter 231: http://eaa231.org
>Ultralights: http://usua250.org
>VA EAA State Fly-in: http://vaeaa.org
>_______________________________________
>to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
>please see other KRnet info at http://www.krnet.org/info.html

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