maybe I have some input. At one time I owned two KR's. one a stock original 
retractable and the other a pretty turbocharged fixed gear KRIIS. Both handled 
about the same. Didn't need both. I have never regretted keeping funky old 
81JM. 
Ken got it right the first time.--
Sent from my Alcatel A405DL

KRnet wrote:
> I should have mentioned that Ron Wanttaja wrote a Kitplanes article on tail 
> volume  about 20 years ago while I was building my KR2S fuselage, and got me 
> thinking about that and the KR2's reputation for being pitch sensitive in 
> flight.  He created a chart with about 20 airplanes on it, along with their 
> calculated horizontal tail volume coefficients.  If the KR2 was added to that 
> list, it would have been dead last by a large margin, with the KR2S somewhat 
> better, thanks to the extra 14" bay that was added.  I have that chart saved 
> somewhere, and will post it when I come across it again.
>
> Now I'm not saying that KRs are unflyable, not at all.  I just thought I'd 
> stack the odds in my favor while I was building mine, and am quite happy with 
> the results.  Any plane as small as these is going to be more sensitive than 
> a larger plane (all other things being equal), but the small tail makes it 
> worse.  Widening the horizontal stab is enough enough....you can do it with 
> mere foam and carbon fiber like Troy did. It's arguable that a stress riser 
> is created that would increase stress of the horizontal stab spars, but if 
> you put enough vertical force on that tailplane, you are already done for, I 
> suspect.
>
> Mark Langford
> m...@n56ml.com
> http://www.n56ml.com
> Huntsville, AL
>
> On 2/4/2021 8:50 AM, Mark Langford via KRnet wrote:
>> Larry Flesner wrote:
>>>  > Questiion.  Was and by how much was the tail area enlarged in the 2S
>>
>>  > over the KR2?  Mark, was your tail volume enlarged over the 2S?  If
>>  > anyone has the numbers I'd be curious how my standard KR2 tail area on a
>>  > 24" stretch fuselage compares the the 2S.
>
>>> Yes, my plane is more stable as a result of the longer horizontal stab, > 
>>> plus the extra few inches added to the fuselage, and the more forward > 
>>> sweep to my wings (due to adapting the new airfoil to the existing > 
>>> spars).   See the link below for details and how to figure it out.
>>>   I calculated all that stuff for the KR2 vs the KR2S twenty years ago > or 
>>> so, but am too busy (and lazy) to do it again.  I got this from > Pazmany's 
>>> book, which the link below refers to.  I can definitely say > that my KR2S 
>>> (and most others, I'm sure) is  a lot more stable than the > KR2 that I'm 
>>> now flying, and the KR2 has a "forward of center" CG almost > all the time.
>>> See link:
>>
>> https://www.eaa62.org/technotes/tail.htm#:~:text=For%20the%20Vertical%20Tail%20Volume,area%20and%20b%20%3D%20wing%20span
>>  > > > Mark Langford
>> m...@n56ml.com
>> http://www.n56ml.com
>> Huntsville, AL
>
>>>> _______________________________________________
>>>
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