Carbon Fiber, Virtual coupon test (90-10-0 degree)
This is an example of tensile loading of carbon fiber/epoxy matrix composites we simulated using MultiMech. The models consisted of coupons with the same shape, but three different fiber orientations - 0 degrees (aligned to the loading direction), 10 degrees and 90 degrees (perpendicular to the loading). Different failure patterns can be observed, both when comparing orientations and between different regions of the same coupon. Failure mechanisms reproduced are consistent with actual crack morphology. Note, the highly accurate Fiber/Matrix interface debonding moment and its capture by MultiMech.
Thank you to Solvay for helping with the materials side of this research.
Please come review our capabilities: www.MultiMechanics.com
Atlantis by Audionautix is licensed under a Creative Commons Attribution license (https://creativecommons.org/licenses/by/4.0/)
Artist: http://audionautix.com/
This is an example of tensile loading of carbon fiber/epoxy matrix composites we simulated using MultiMech. The models consisted of coupons with the same shape, but three different fiber orientations – 0 degrees (aligned to the loading direction), 10 degrees and 90 degrees (perpendicular to the loading). Different failure patterns can be observed, both when comparing orientations and between different regions of the same coupon. Failure mechanisms reproduced are consistent with actual crack morphology. Note, the highly accurate Fiber/Matrix interface debonding moment and its capture by MultiMech.
Thank you to Solvay for helping with the materials side of this research.
Please come review our capabilities: www.MultiMechanics.com
Atlantis by Audionautix is licensed under a Creative Commons Attribution license (https://creativecommons.org/licenses/by/4.0/)
Artist: http://audionautix.com/
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