The aeroelastic stability characteristics of a ring-stiffened conical three-layered sandwich shell with an FG auxetic honeycomb core utilizing zig-zag shell theory-Reference-Cited by-同舟云学术

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The aeroelastic stability characteristics of a ring-stiffened conical three-layered sandwich shell with an FG auxetic honeycomb core utilizing zig-zag shell theory

Published:2024-12 Issue: Volume:155 Page:109551
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Abasi Maryam^ORCID,Arshadi Khashayar,Rafiei Masoud,Afshari Hassan^ORCID

Publisher

Elsevier BV

Reference58 articles.

1. A nonlocal higher-order shear deformation approach for nonline ar static analysis of magneto-electro-elastic sandwich Micro/Nano-plates with FG-CNT core in hygrothermal environment;Anh;Aerosp. Sci. Technol.,2024

2. Nonlinear post-buckling of CNTs reinforced sandwich-structured composite annular spherical shells;Manh;Int. J. Struct. Stab. Dyn.,2020

3. Analytical investigation of in-plane and out-of-plane elastic properties of bone-inspired cellular structures;Van Thuong;Aerosp. Sci. Technol.,2024

4. Honeycomb Technology: Materials, Design, Manufacturing, Applications and Testing;Bitzer,1997

5. Elastic constants of 3-, 4-and 6-connected chiral and anti-chiral honeycombs subject to uniaxial in-plane loading;Alderson;Compos. Sci. Technol.,2010

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