Layout of a shear stiff Panel


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Skout
Skout
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Hello,

for my roadster (1100 kg), which is frequently used on the racetrack, i want to replace the separating sheet metal between the boot and the convertible roof room.
Pictures: http://www.pic-upload.de/gal-703069/7v69gx/1.html

Beside the weight reduction, my target is to enhance the torsional stiffness of the hole car at the rear end.
My solution would be a laminate which combines the shear field theory (panel connected to frame structure) and a frame construction with diagonal braces to use the benefits of the unidirektional fiber placement at reduced material costs.
The following laminate setup is planned:
layer 1 - 200 g/m^2 Carbon Fiber Twill Weave - 0/90
layer 2 - 200 g/m^2 Carbon Fiber Twill Weave - +/- 45
layer 3 - 140 g/m^2 Carbon Fiber UD Tape width ~ 50 mm for every frame brace
layer 4 - 140 g/m^2 Carbon Fiber UD Tape ...
layer 5 - 140 g/m^2 Carbon Fiber UD Tape ...
layer 6 - 140 g/m^2 Carbon Fiber UD Tape ...
layer 7 - 200 g/m^2 Carbon Fiber Twill Weave - +/- 45
layer 8 - 200 g/m^2 Carbon Fiber Twill Weave - 0/90

Would the laminate setup be enough shear stiff and have you suggestions for:
- the number of layers,
- ply weights,
- the laminate setup an strength theory layout in general,
- and especially choosing the right frame structure for optimal force paths ?

The clearance holes will be stung in the dry fabric and the distance to edges will be increased.
The frame nodes will be crossing UD tapes, so the laminate would gain twice the thickness at the clearence holes for enhanced application of force.
Another benefit of the planned laminate setup could be that it has less denting danger.
Production via resin infusion on a mould with the original geometry.
With the use of expensive carbon fiber, i would like to achieve a stiffer sheet/panel right in the first try.

Greetings from Germany,
Alexander
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ChrisR
ChrisR
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It looks like you are still thinking in metal terms.

If you are looking for torsional & shear stiffness (in the laminate plain) but still want carbon weave for looks then I'd be looking at something like:

200gsm woven (twill or plain your preference)
150/140 +/- 45 UD over the entire part (or 300 bi-ax)
3mm core
150/140 +/- 45 UD over the part (or 300 biax)
150/140 0 UD

I'd recommend you do a trial section to check but you shouldn't really need to balance the layup in this as the stiffness of the bi-ax / UD will be significantly greater than the surface layer of the 200 woven. You'd be best to post cure at 60-80deg for a few hours (resin dependent) and control the cool cycle to reduce any distortion from the uneven layup.

plus add hard points i.e. multiple layers of UD/woven at the mountings

If you are intent on having "cross bracing" and significantly adding stiffness then look at something like this:

200 woven
0/90 UD
50mm wide 6mm core strips with 0/90 UD wrap (with core strips at +/-45)
+/- 45 UD
0/90 UD





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