Here's Don Stackhouse's Q&A site URL:
http://www.djaerotech.com/dj_askjd/

-Lloyd Schultz

Ron Freiberger wrote:

> Most of that crap is smoke and mirrors.  Anyone who thinks lengthening the
> tail 14 inches will fix it probably also believes in Leprechauns.  I don't
> tell my leprechaun story lightly.
>
> Ron Freiberger
> mailto: rfreiber...@swfla.rr.com
>
> -----Original Message-----
> From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On Behalf Of
> Oscar Zuniga
> Sent: Tuesday, June 03, 2003 12:30 PM
> To: kr...@mylist.net
> Subject: KR>it's something to do with the elevators
>
> Ameet writes-
>
> >When the distance between the HS and the wing is small (short couple) like
> >in the KR
> >the NP is close to the surface with the higher lift (the wing) which leaves
> >less
> >static margin for the CG and hence the inherent pitch sensitivity.
>
> If any airplane should be short-coupled and pitch sensitive (just by
> observation), it would be the Questair Venture.  But it isn't (read the
> flight test info at http://www.airbum.com/pireps/PirepQuestairVenture.html )
> so it must be "something to do with the elevators" ;o)  Far better minds
> than mine have tackled this issue and have come up with redesigned tails,
> aerodynamic counterbalances, different linkage ratios, biasing springs, and
> other things to change the pitch feel of the KR, and the jury is still out
> on many of these things because they haven't flown yet.  But I'll bet that
> by this time next year there will be some actual data posted here, so stay
> tuned.
>
> Oscar Zuniga
> San Antonio, TX
> mailto: taildr...@hotmail.com
> website at http://www.flysquirrel.net
>
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