Sorry, but I don't have a good solution for replacing the longerons, but I can
show you why you have the cracks in the place you have them. If you look at the
two bottom images on this side http://go-design.no/images2.html, you can see
that the curvature on the original drawings is high in
On 12.07.2010 15:53, Gunnar Olsen wrote:
> For a straight wing tapering from 48 to 36 inches; when quarter chord
> sweep is straight, the leading edge of the tip spar is 3 inches behind
> the leading edge of the root spar.
>
> It does not matter where the actual wing spar is located
For a straight wing tapering from 48 to 36 inches; when quarter chord
sweep is straight, the leading edge of the tip spar is 3 inches behind
the leading edge of the root spar.
It does not matter where the actual wing spar is located and what angle
it has. ( but I believe on the KR it should be
KR2 standard wing with RAF48 airfoil.
Dihedral at bottom of wing: 3.64 deg.
Dihedral at wing chord: 3.05 deg.
Dihedral at wing center: 2.93 deg.
Dihedral at top of wing: 2.21 deg.
;o) Gunnar
On 30.06.2010 12:12, phillip matheson wrote:
> What is the degree of dihedral on the KR2?
>
>
> Dan
For the plans, you could try
http://thepiratebay.org/torrent/4907244/Home.Built.Ultralight.Airplane.Rand.Robinson.KR-1.Plans.V1.0.rar
I think it is quite complete.
/Gunnar
On 20.06.2010 00:41, Jacob Choitz wrote:
> Hi, im new to kr net and i am trying to figure out how to post a wanted ad. I
Hi all,
Does anyone know the differences in weight and (engine) cg location of a
VW (Aeroconversions 2180) and an O200 installation ?
Regards
Gunnar
Hi Todd,
Look forward to see your new design. I'm doing the same thing myself.
If you want to, I can host your images on my site
http://www.go-design.no/index.html or http://images.go-design.no/
Regards
Gunnar Olsen
Siljan, Norway
Todd Price wrote:
> OK that didn't work. Need to
Welcome to the list, and the best source of KR information, John.
I have not seen anything about v tails before, as for the airfoil, I
think this will explain most of it.
http://www.krnet.org/as504x/
Best Regards
Gunnar Olsen
Siljan, Norway
> a.) Has there ever been any discussion ab
Hi guys,
Good to see that you got the graphic you asked for Todd.
Thanks for all nice comments to my cad model. Hopefully (with a lot of
work) my KR will look equally nice when finished.
--
Gunnar Olsen
Siljan, Norway
Darren Crompton wrote:
> Hi Gunnar.
>
> Just a quick email t
Sorry, not exactly... but will have in a short while -
http://www.go-design.no/images.html
It's not exactly per plans, it's quite near though.
Beast Regards
Gunnar Olsen
Siljan, Norway
Todd Price wrote:
> Does anyone have a larger graphic of the kr2 like the one on the KR Net
> logo?
>
>
Hi, and thanks for all feedback.
Looks like the Bingelis books are the ones to get then.
I've seen some of the videos on the EAA site, great resource there as well.
Best Regards
Gunnar Olsen
member, EAA chapter 573 (Norway) :o)
Larry Flesner wrote:
> I forgot to mention the great vid
Hi All,
I have looked through a LOT of webpages and found several books to read
before starting a new (first) project. My list of books are now getting
long ... very long...
The big question is now: What book(s) are generally known to be the
homebuilders "bible", that has the most useful
and experiences, it would be
highly appreciated
Thanks !
Best Regards
Gunnar Olsen
I try to reach Rand Robinson Engineering for buying a set of KR-2S
plans, but get no answer on neither fax nor phone.
Any suggestions anyone ?
Thanks.
Gunnar
x Generators
Thanks Dan ! I will try them as well. They reduce stall speed by 8-9 %
on a C172, so they certainly helps.
Regards
Gunnar Olsen
KIAS (40mph)
My question: Is it possible to get the Vn0 down to 35KIAS with the help
of flaps / winglets etc. ?
All help and suggestions are highly appreciated.
Thanks !
Best Regards
Gunnar Olsen
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