On 10/7/2021 8:55 PM, Global Solutions wrote:
Can anyone shed some light on how far one can fly with a kr2S with 140 lbs pilot and full tanks and a 110 hp Corvair engine?
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usable fuel on board  /  fuel burn per hour X ground speed = distance,  Increase range by adding tankage.   simple math.  Keep additional tanks as close to the CG envelope as possible, i.e., build wing tanks long and narrow and close to the main spar.  Being experimental the tankage is up to the builder and almost everyone is different and often more than is needed.

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Has anyone built solid wing spars instead of boxed hollow spars for their
KR?
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Yes. I did.

Weight increase 12 lbs

strength and flex  increase  close to 2x
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Is that claim a "design calculation" or "test to destruction" test?  Have the stress 
points changed anywhere in the wing?  Having watched a standard spar tested to destruction (video on the net) 
I question the "2X flex".  Additionally, why is anyone trying to increase the strength of a wing 
that has been flight tested to at least 6G's on an airplane that was 760 pounds empty with a 200+ pound pilot 
that accidentally fell out of an aerobatic maneuver? (Marty Roberts)  The KR doesn't need to be any stronger 
than Ken and Stu designed it 50 years ago. You're going to end up heavier than you want anyway.  Don't add 
unnecessary weight.

This answer is not meant to stop discussion but but sometimes we builders get 
off in to the weeds unnecessarily. Any claims such as the above should be 
supported with valid proof for safety reasons.

Larry Flesner





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