Aeroelastic analysis of foam-filled composite corrugated sandwich plates using a higher-order layerwise model
Author:
Publisher
Elsevier BV
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference48 articles.
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3. Glass DE. Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles. Proceedings of 15th AIAA Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, 28 Apri-1 May 2008.
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5. Integrated thermal protection system based on C/SiC composite corrugated core sandwich plane structure;Li;Aerospace Science and Technology,2019
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1. Aeroelastic analysis of a lightweight topology-optimized sandwich panel;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-05-10
2. Vibration Characteristics and Aeroelastic Stability Behavior of Foam-Filled Composite Corrugated Sandwich Panels Considering Mass Reduction;Journal of Aerospace Engineering;2024-03
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4. Vibration and aeroelastic stability analysis of hexagonal honeycomb core sandwich panels in supersonic airflow;Thin-Walled Structures;2022-11
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