Chickenhawk
Agricultural
I have constructed an experimental aircraft spar of wood and pultruded carbon fibre. The wood core is 1/2" by 1" and two flat rods (0.092"*0.220" are epoxied flat side down, side by side, on both top and bottom wood surfaces. The spar is lightly loaded in vertical shear which is handled by the wood core. The spar caps of pultruded fiber have been loaded succesfully to twice the max. bending moment. Axial load between compression struts is the most critical loading factor and the buckling tendency is taken care of by additional epoxied carbon fibre strips in the critical areas on the sides of the spar. FEA analysis indicates all is well. I would like to ensure against delamination of the fibre rods from the wood by wrapping an epoxied fibre tow around the spar but not to the extent that the fibre takes the shear and not completely enclosing the spar. Like wrapping at 45° diag. one way with a matching 45° the opposite. Or just vertical wraps at 3" centers or so. Any suggestions as to how to accomplish this without shear problems in the fibre would be appreciated.