Yes, there were quite a few analysis done on the KR and references and part 
excerpts can be found in the KR newsletter. I also know that the plans in the 
past have been slightly updated to reflect the "weak" points (as found in the 
analysis) in the design, which were a reinforced web structure at the empanage 
and addition of an addition V-brace on the top of one of the fuselage bays. The 
spars, fittings and everything else has been found to be very strong as 
attested in the very few if any breakups when looking through the NTSB reports. 
It was also recommended to use reinforcement aluminum channels at the front if 
larger engines i.e. the 80 hp is used KR 2 (no larger engines are 
recommended!!!!!  as the increased weight requires structural changes resulting 
in......). KR 2 S is different and beyond my experience.

I also want to point out that Ken Rand was an aeronatical engineer and was very 
capable of designing this aircraft. Second guessing the design after hundreds 
or close to thousand flying KR's does not help to instill confidence in our 
cause.

Regards,
Harold

larry severson <lar...@socal.rr.com> wrote:
At 05:47 PM 6/23/2004 -0400, you wrote:
>Did you ask her why you can't get the complete analysis? Can you get any
>part of the analysis?

The KR is a radio control model scaled up to one carrying people. It was 
not "engineered" at any time. The critical factor in the design is the wing 
spars vs the weight and G loading. Calculation of this information is 
fairly trivial with formulas in many book, including at least one high 
school physics book by Saxon Publishing.

Of course, another factor is having a strong enough front end to support 
the chosen engine.

Bottom line, don't waste time looking for a structural analysis - it 
doesn't exist, at least not from Rand Robinson and Jeanette isn't trained 
to do one.


Larry Severson
Fountain Valley, CA 92708
(714) 968-9852
lar...@socal.rr.com 


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