Several causes of flutter. However, any malformation of
the elevator, depends on the malformation. Exceeding
Vne coupled with excess loading factor and all bets are off.

----- Original Message ----- 
From: "larry flesner" <fles...@midwest.net>
To: "KRnet" <kr...@mylist.net>
Sent: Thursday, March 18, 2004 5:14 AM
Subject: KR>aircraft performance / balanced elevator


> I am interested in what speeds
> >aircraft are attaining with out mass balancing of the elevator as my
> >elevator is built and what peoples oppions are as flutter can be destroy
an
> >aircraft inflight!
> >Ross
> ++++++++++++++++++++++++++++++++++++++++++++++++++++++
>
> Ross,
>
> I think a lot of apples and oranges are being mixed here.
>
> Flutter can happen at any speed and is not JUST speed related although
> speed can be a major factor.  The engine size is irrelevant to flutter
other
> than it's relation to speed and finally, balancing the elevator has
nothing
> to do with aircraft stability other than the probably modest affect on CG.
>
> I"m using an 0-200 and because of several variables my KR is slower than
> most using that engine.  Without wheel pants I'm getting a solid 150+ mph
> cruise.  I'm in the middle of the CG envelop with me ( 200 lbs) and full
> fuel (25 gal in wings, no header).  My plans size trim tab seems to be
> suffecient in the CG range I'm flying in but a similar KR which flies in
> the forward part of the CG range runs out of trim authority with a
standard
> size tab.  I think the standard size KR2 with an 0-200 is probably getting
> close to an honest 180 mph cruise and the 0-200 will probably burn
> 5.5 to 7.5 gal per hour, depending on the power setting.
>
> The elevators can be externally balanced and made to look good.
> Weights can be added to the ends of the elevator and extend
> forward along the edge of the horizontal stab.
>
> As to the Vne, I'd guess there are more factors limiting the Vne than
> elevator flutter but hey, I'm not an engineer.
>
> I almost forgot, I did balance my elevators.
>
> Larry Flesner
>
>
>
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