Craig,
With the general consensus leaning toward increasing the size of the 
horizontal stabiliser and in turn the control surface area I'd advise 
you get the concept of reducing the elevator size checked thoroughly 
before you decide to run with it. for 2 reasons.
1. Because the KR is so closely coupled the wings can blanket part of  
the horizontal at high angles of attack, the width of the elevator 
allows part of the control surface to protrude outside of this effect 
and allow controllability in these attitudes.
2. The elevator is effectively altering the airfoil and angle of attack 
of the horizontal stabiliser to perform it's task, too great a 
deflection could result in a stalling of the stabiliser with unwanted 
results.
Please be sure to have your ideas thoroughly vetted before implementing 
them.
Cheers.
Pete Bancks.
Ballina.
Oz.

On 18/10/2010 10:26, Craig Williams wrote:
> My Bad.  I opened my big mouth without running the numbers first.  Here are 
> the
> #'s
>
> The tail as bought from the previous owner.  H/S is 827 sq in and the elev is
> 827 sq in.  If I use this tail I will add 100 sq in to the HS to round the
> ends.  The previous builder added lead shot in the elev to add a 
> counterweight.
> Mine will be internal so this will be removed at the ends.  This would remove 
> 84
> sq in of the elevator.  The difference between the added area to the H/S and 
> the
> removal of the weight from the elev will effectively be a 20% change in the
> ratio of the area of the H/S to the elevator area.  Also my elev controls are
> going to be adjustable so I can increase the throw of the elevator if I need
> to.  This is a small change in area and I believe the effects on controlling 
> the
> plane will be positive.  Most landing will be two wheelers with the speed 
> brake
> deployed.  Hope this helps
>
> Craig
> www.kr2seafury.com



Reply via email to