KirbyWan
Aerospace
- Apr 18, 2008
- 586
Howdy all,
I'm going to lay up some test panels of carbon fabric with EA9390 adhesive and cut tensile test coupons to compare strength. I'm going to make three panels of 3K-70-PW (8 plies), 3K-135-8H (4 plies) and AH370-5H (4 plies). I was wondering If there is a difference between the 0° and 90° direction for a fabric with the same number of tows per inch in each direction and the same fibers per tow. Should I lay up the panel with all laminae in the same direction? Should I alternate back and forth? If I lay up the panel with all laminae in the 0° direction should the test coupons pull the same if cut in the 0° vs 90° direction?
My intuition is that they should be identical regardless of ply laminate direction and test coupon direction as long as it's parallel to one of the fiber directions, but I wanted to check with this august and knowledgeable forum for their expertise.
Thanks,
-Kirby
Kirby Wilkerson
Remember, first define the problem, then solve it.
I'm going to lay up some test panels of carbon fabric with EA9390 adhesive and cut tensile test coupons to compare strength. I'm going to make three panels of 3K-70-PW (8 plies), 3K-135-8H (4 plies) and AH370-5H (4 plies). I was wondering If there is a difference between the 0° and 90° direction for a fabric with the same number of tows per inch in each direction and the same fibers per tow. Should I lay up the panel with all laminae in the same direction? Should I alternate back and forth? If I lay up the panel with all laminae in the 0° direction should the test coupons pull the same if cut in the 0° vs 90° direction?
My intuition is that they should be identical regardless of ply laminate direction and test coupon direction as long as it's parallel to one of the fiber directions, but I wanted to check with this august and knowledgeable forum for their expertise.
Thanks,
-Kirby
Kirby Wilkerson
Remember, first define the problem, then solve it.