Dihedral is solely for lateral stability. You sacrifice just a little bit of lift for stability. It sounds like you kept the same angle...and that is good. Make sure you maintain the washout...that is there to make the outboard wings and ailerons stall last...again for lateral stability.
Decalage is never "correct". You have to have downlift on the stabilizer to maintain pitch stability. The decalage is there as a neutral difference in stab aoa and wing aoa for level flight...but that changes with gross weight, cg, and airspeed. Logically a longer fuselage would drive less aoa on the stab to get the same moment. https://sites.google.com/site/mykr2stretch/ https://sites.google.com/site/mykr2stretch/parts-for-sale On Jun 11, 2014 7:00 AM, "cruzj12--- via KRnet" <krnet at list.krnet.org> wrote: > Good mornignKR builders, > I have a question about wing dihedral for all the aeronautical engineering > people here.I'm currently extending my carbon fiber wing extensions with > the 29" template on the ends. My Fuselage is 18" longer than a standard > KR2S. . I'm measuring 5.25" of dihedral at the end of the main wood spars. > Is the extra quarter inch of dihedral going to affect the declage in favor > or not . With the tail 18" farther back it seems the decalage will be > smaller. My tail feathers are adjustable so I have ability to make > adjustments .Is more dihedral a more advantage in my case or not? Thanks > for any advice > Joe Cruz > cruzj12 at frontiernet.net > KR1.5 N3151K > KR2S builder > _______________________________________________ > Search the KRnet Archives at http://tugantek.com/archmailv2-kr/search. > To UNsubscribe from KRnet, send a message to KRnet-leave at list.krnet.org > please see other KRnet info at http://www.krnet.org/info.html > see http://list.krnet.org/mailman/listinfo/krnet_list.krnet.org to change > options >