If you do it right, you should not impose more than 1g on the airframe in a roll.
Jeff On 3/12/07, Larry&Sallie Flesner <fles...@verizon.net> wrote: > At 07:50 AM 3/12/2007, you wrote: > >For my own knowledge were does the # 5600 come from. > +++++++++++++++++++++++++++++++++++++++++++++++ > > + / - 7G's at 800 pounds. > > 7 X 800 = 5600 pounds = design maximum weight the > structure will carry. If your KR weighs 1000 pounds, the > structure will still only carry 5600 pounds so 5.6 G's > will place you at the 5600 pound limit. Since the weakest > point seems to be where the wing attach fittings attach to > the spar, the only way to really know what your structure > will support would be to test to failure. I don't see that > in my future. :-) > > Larry Flesner > > > _______________________________________ > Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp > to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net > Post photos, introductions, and For Sale items to > http://www.kr2forum.com/phpBB2/index.php > please see other KRnet info at http://www.krnet.org/info.html >
