The bend would be at the fuselage-stub-wing joint. I've got another project (Turner T-40) that uses such a design - a solid center-spar of laminations, bent at a 5-degree angle on each side, where the side exits the fuselage.
On 2/9/2012 7:18 PM, GaryH wrote: > Bill, > This is an interesting thought and I like the idea. Where would the "bend" > be located along the spar? How would you carve or contour the foam over a > complex curve? > > Anyone, > On another note, I've read in the plans that one layer of 5.6 oz glass cloth > is used for covering. It seems this is a bit light. What has been > everyone's experience? > > Regards, > Gary > > > > > > > -----Original Message----- > From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf > Of ol' weirdo > Sent: Thursday, February 09, 2012 8:01 AM > To: KRnet > Subject: KR> solid centre wing spar > > Mr. Wade, If you are going to build a solid centre wing spar of laminates > you might bend them so there is no change of angfle where the outer wing > panels joins the centre section. > > Bill Wer > _______________________________________ > Search the KRnet Archives at http://mylist.net/private/krnet/ > to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net > please see other KRnet info at http://www.krnet.org/info.html > > > _______________________________________ > Search the KRnet Archives at http://mylist.net/private/krnet/ > to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net > please see other KRnet info at http://www.krnet.org/info.html
