Assessment of Damage Tolerance and Static Residual Strength of Z-Pin Reinforced Composites
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1044
Reference4 articles.
1. Low-Velocity Impact Damage and Delamination Crack Arrestment with Translaminar Reinforcements
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1. Damage tolerance related to the damage area of impacted carbon/epoxy composite laminates;Journal of Composite Materials;2023-06-05
2. Damage mechanisms in the CAI failure of thin z-pinned composite laminates;Composites Part A: Applied Science and Manufacturing;2022-07
3. Design of a Fail-Safe Crack Arrested Test Specimen for Certification of Bonded Unitized Composite Structures;AIAA SCITECH 2022 Forum;2022-01-03
4. The Use of LS-DYNA MAT299 for Accurate Prediction of Impact Damage in Composite Structures;AIAA Scitech 2021 Forum;2021-01-04
5. Modeling the Compression-after-impact Behavior of a Z-pinned Composite Laminate;AIAA Scitech 2021 Forum;2021-01-04
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