Optimal Design of a Composite Sandwich Panel with a Hexagonal Honeycomb Core for Aerospace Applications
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,Computational Mechanics
Link
https://link.springer.com/content/pdf/10.1007/s40997-022-00520-1.pdf
Reference42 articles.
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3. Anish, Kumar A, Chakrabarti A (2019) Failure mode analysis of laminated composite sandwich plate. Eng Fail Anal 104:950–976. https://doi.org/10.1016/j.engfailanal.2019.06.080
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5. Arunkumar MP, Pitchaimani J, Gangadharan KV, Leninbabu MC (2018) Vibro-acoustic response and sound transmission loss characteristics of truss core sandwich panel filled with foam. Aerosp Sci Technol 78:1–11. https://doi.org/10.1016/j.ast.2018.03.029
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