Finite Element Analysis of Eddy Current Testing of Aluminum Honeycomb Sandwich Structure with CFRP Panels Based on the Domain Decomposition Method
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s10921-024-01053-0.pdf
Reference12 articles.
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3. Schaal, C., Tai, S., Mal, A.: On the assumption of transverse isotropy of a honeycomb sandwich panel for NDT applications. SPIE Conf. Health Monitor. Struct. Biol. Syst. 10170, 2260092 (2017). https://doi.org/10.1117/12.2260092
4. Wang, Y., Cheng, W., Wang, S.: Review of the application of composite honeycomb sandwich structure on civil aircraft. Fiber Composites. 38(2), 73–77 (2021). https://doi.org/10.1016/j.jcomc.2020.100004
5. Wang, J., Shi, C., Yang, N., Sun, H., Liu, Y., Song, B.: Strength, stiffness, and panel peeling strength of carbon fiber-reinforced composite sandwich structures with aluminum honeycomb cores for vehicle body. Compos. Struct. 54, 2159–2171 (2017). https://doi.org/10.1016/j.compstruct.2017.10.038
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