Out-of-plane Properties and Failure Mechanism of Composite Laminates Reinforced With Carbon Z-pins
Author:
Funder
Fundamental Research Funds for the Central Universities
Publisher
Springer Science and Business Media LLC
Subject
Ceramics and Composites
Link
https://link.springer.com/content/pdf/10.1007/s10443-022-10087-4.pdf
Reference43 articles.
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2. O’Brien, T.K., Krueger, R.: Influence of compression and shear on the strength of composite laminates with z-pinned reinforcement. Appl. Compos. Mater. 13, 173–189 (2006). https://doi.org/10.1007/s10443-005-9005-4
3. Debout, P., Chanal, H., Duc, E.: Tool path smoothing of a redundant machine: Application to Automated Fiber Placement. Comput. Aided Des. 43, 122–132 (2011). https://doi.org/10.1016/j.cad.2010.09.011
4. Choi, H.S., Ahn, K.J., Nam, J.D., Chun, H.J.: Hygroscopic aspects of epoxy/carbon fiber composite laminates in aircraft environments. Compos. Pt. A-Appl. Sci. Manuf. 32, 709–720 (2001). https://doi.org/10.1016/S1359-835X(00)00145-7
5. Chen, X., Zhao, W., Zhao, X.L., Xu, J.Z.: Failure Test and Finite Element Simulation of a Large Wind Turbine Composite Blade under Static Loading. Energies 7, 2274–2297 (2014). https://doi.org/10.3390/en7042274
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