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Archive of Applied Mechanics

Erschienen in:

11.07.2022 | Original

Numerical and experimental deflection behavior of damaged doubly curved composite laminated shell structure

verfasst von: Vikash Kumar, Hukum Chand Dewangan, Nitin Sharma, Subrata Kumar Panda

Erschienen in: Archive of Applied Mechanics | Ausgabe 10/2022

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Abstract

The deflection behavior of laminated shell structure with combined damages (crack/delamination) under mechanical loading is presented numerically and verified with subsequent experimental results. In this article, the damaged layer structure is modeled mathematically using higher-order (third-order) polynomials and the finite element method. The variational method is employed to obtain the final governing equation for the shell model. The results are obtained computationally using a computer code developed in a MATLAB environment. The consistency of the current mathematical model is confirmed by performing a convergence test, and the model's validity is checked further by equating the solution with published data in the open domain. Finally, some examples are presented to observe the combined effect of delamination (various shapes and sizes) and/or crack (different orientations), including various input parameters (modular ratio, curvature ratio, thickness ratio, boundary restriction) on the deflection behavior of laminated curved shell structure under mechanical loading.

Vorheriger Artikel T-stress for the central cracked Brazilian disk under non-uniformly distributed pressure

Nächster Artikel A new bending model for composite laminated shells based on the refined zigzag theory

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Titel: Numerical and experimental deflection behavior of damaged doubly curved composite laminated shell structure
verfasst von: Vikash Kumar
Hukum Chand Dewangan
Nitin Sharma
Subrata Kumar Panda
Publikationsdatum: 11.07.2022
Verlag: Springer Berlin Heidelberg
Erschienen in: Archive of Applied Mechanics / Ausgabe 10/2022
Print ISSN: 0939-1533
Elektronische ISSN: 1432-0681
DOI: https://doi.org/10.1007/s00419-022-02202-5

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