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Culver General Discussion / Re: New wings for the Culver Cadet
« on: June 13, 2012, 09:48:42 PM »It is interesting to note that in ANC-18 (Design of Wood Aircraft Structures, 1944) on page 235 &236 the Cadet spar was the subject of at least 5 test loadings to failure with modifications between each. The production spar, it appears, was loaded to failure at a moment of 174138 in. lbs. on the fuselage (outboard) attach bolt.
Paul,
I may have spoken prematurely to modifications of the Culver Cadet spar design. Any chance you could scan copies of the pages relevant to the Cadet? The only downloadable versions of ANC-18 I've been able to find online end at page 234.