Geometrically nonlinear analysis of sandwich panels with auxetic honeycomb core and nanocomposite enriched face-sheets under periodic and impulsive loads-Reference-Cited by-同舟云学术

Geometrically nonlinear analysis of sandwich panels with auxetic honeycomb core and nanocomposite enriched face-sheets under periodic and impulsive loads

Published:2023-04 Issue: Volume:135 Page:108195
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Mirfatah Sayed Mohamad^ORCID,Tayebikhorami Saman,Shahmohammadi Mohammad Amin,Salehipour Hamzeh,Civalek Ömer^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference65 articles.

1. Effects of nonlinear strain components on the buckling response of stiffened shear-deformable composite plates;Ruocco;Composites, Part B, Eng.,2015

2. Free vibration analysis and optimization of doubly-curved stiffened sandwich shells with functionally graded skins and auxetic honeycomb core layer;Pham;Thin-Walled Struct.,2022

3. Higher order formulations for doubly-curved shell structures with a honeycomb core;Tornabene;Thin-Walled Struct.,2021

4. Free vibration response of auxetic honeycomb sandwich plates using an improved higher-order ES-MITC3 element and artificial neural network;Pham;Thin-Walled Struct.,2022

5. Effective elastic properties of periodic hexagonal honeycombs;Malek;Mech. Mater.,2015

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