Valid points, but not essential for the main issue which is achieving enough stiffness for the strut. I don't think hitting the strut is a very big thread, front wing/fuselage comes first and takes most of the hits.plummet wrote:If manually shaping it will make for an easier transition and wont expose the core when shaping the mast.
Also it will provide impact resistance if the mast is hits something. There would be less likelyhood of core being exposed.
I meant weaved carbon material, a kind of sock of carbon which can adapt to different thicknesses. Then fiber direction will change but it is not so precise, in "neutral" position fibers are at 45 degrees. I think this material makes it possible to have a very nice outer surface (seamless) for tubular carbon parts, and of course it gives strength/stiffness. But I haven't tried it.downunder wrote:Yes, a carbon tube is fine but again, not so for torsion. There is no 45 degrees carbon tube that I can find.
Yes, then two layers, it makes layers crossing on both sides which is good, torsional stresses dividing symmetrically in both sides of the strut. I have done some glass/carbon parts on foam core and noticed 45 degree UD wrapping gives as much torsional rigidity as needed.downunder wrote:We can definitely wrap with more 45 degrees carbon but 1 layer each side is not enough from my tests.
For the box beam I agree, but at the skin of the strut shear is not a problem. So I wouldn't use more than one layer of biax there and even that mostly for aesthetics. Straight and 45 degree UD should be enough, 45 degree carbon gives chordwise strenght very probably enough. Now I just don't see why straight fibers from LE to TE should be there.foam-n-fibre wrote:a box type tube of biax the fibres of the carbon are better aligned to support shear (sliding of one side up or down compared to other side as strut flexes). Also I think having those fibres wrap onto the skin is helpful.
If some internal structure for the strut is needed I would suggest the hollow beam in the center, then adding LE and TE parts (with or without carbon) and finally wrapping UD carbon straight and 45 degrees to finish. I think it is better than surface structure, but also more laborous.