by GreenLake » Mon Jun 22, 2009 4:27 am
Very interesting.
How were you determining that "stiffness"? By pushing at the hull from below? Because that would put tensile stress on the inside, having a carbon layer there should help.
BTW, in my reading on out of plane loads on hull panels, I came across something interesting: that such panels can act like membranes - in other words, both surfaces are under tension. Unlike a beam, where the inner surface (in relation to the bending curvature) would be compressed.
Changing such a membrane by adding a layer that's significantly better at resisting tension ought to be noticeable - you are saying it is.
Your carbon fabric should stretch, what, 2-5 times as little for the same load compared to the glass? If we assume that section of the hull acts as a membrane where the entire laminate is under tension, the existing glass contributes. If you add more glass, then the effect is simply proportional to the increase in cross section.
If, let's assume, one layer amounts to 25% of the total laminate, i.e. 4 layers in total, you've added perhaps 33% by using glass. By using carbon you added perhaps 3x33% (or more, depending on the factor) which would be a doubling (or more) of the existing membrane strength.
Now, all of this changes when you add a sandwich. I don't know whether the membrane or the beam model gives a better description of your sandwiched hull, but in a beam style situation adding carbon near the middle (between skin and core) should be least effective, because of geometry.
But, to the degree that the hull acts like a stretched (deflected) membrane, then adding tensile strength to either skin should have some incremental effect.
Unfortunately, I expect that your foam core (even with only glass) is going to be so stiff that you could not readily observe the difference to carbon, as you did with the single added laminate. Would be really interesting.
Keep building, keep observing!
~ green ~ lake ~ ~