Technical Papers
Jul 13, 2024

Designing a Stiffener Layout that Resists the Wrinkling Behaviors of Sandwich Panels

Publication: Journal of Aerospace Engineering
Volume 37, Issue 5

Abstract

Wrinkling is a typical failure mode of sandwich structures with thin skins, where the bending deformation of face skins occurs simultaneously in conjunction with transverse stretching deformation of core layer. To analyze the three-dimensional (3D) deformation of wrinkling, a model is required to possess a capability describing completely different deformations at each ply. Therefore, by utilizing the Chebyshev polynomial at each layer of sandwich panels, this paper focuses on proposing a higher-order model to individually illustrate deformations of the skins and the core. By means of the proposed model, a refined triangular element has been constructed. By analyzing the stability of a sandwich plate without stiffeners, the finite-element formulation has been verified by comparing it to the quasi-3D elasticity solutions. In addition, it is anticipated that wrinkling failure can be effectively restrained by designing the stiffener layout. To this end, the influence of stiffener layouts on wrinkling behaviors of sandwich plates has been investigated in detail, and it is found that the capability of resisting the wrinkling deformation can be obviously improved by designing reasonable stiffener layouts. Moreover, the translation between buckling and wrinkling behaviors of sandwich panels with different stiffeners has been also explored, which can help to better understand wrinkling deformation mechanism. In summary, the proposed model can be used to design a reasonable arrangement of stiffeners to resist the wrinkling failure of sandwich panels.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

The work described in this paper was supported by the National Natural Sciences Foundation of China (No. 12172295).

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 5September 2024

History

Received: Nov 14, 2023
Accepted: Apr 18, 2024
Published online: Jul 13, 2024
Published in print: Sep 1, 2024
Discussion open until: Dec 13, 2024

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Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xian 710072, China; Professor, National Key Laboratory of Strength and Structural Integrity, Shaanxi, Xi’an 710065, China (corresponding author). ORCID: https://orcid.org/0000-0003-4800-5460. Email: [email protected]
Senlin Zhang
Ph.D. Student, School of Aeronautics, Northwestern Polytechnical Univ., Xian 710072, China.

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