Fracture and Structural Integrity e-ISSN 1971-8993 Open access
SI: Fracture Mechanics versus Environment Vol. 13, No. 49 (2019)

Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination

Author and affiliation details
  • AYA BENDADA Corresponding author USTO aya19-23-05@hotmail.fr
  • Djilali Boutchicha Université des Sciences et de la Technologie d’Oran - Mohamed Boudiaf, USTO-MB, Algérie.
  • Adel Chouiter Université des Sciences et de la Technologie d’Oran - Mohamed Boudiaf, USTO-MB, Algérie.
  • Mokhtaria Miri Université des Sciences et de la Technologie d’Oran - Mohamed Boudiaf, USTO-MB, Algérie.
DOI
10.3221/IGF-ESIS.49.59
Pages
655-665
Published
Published inVol. 13, No. 49 (2019)Go to the issue

Abstract

The objective of this paper is to investigate the influence of the delamination on the vibration behavior of honeycomb sandwich panel, firstly, numerical characterization to provide the constant properties of the core only are performed using initial finite element model of Representative Volume Element (RVE) which does not take into account the double thickness wall existing in aluminum core structure. According to these initial parameters, finite element model of sandwich composite plate is constructed to extract its elasto-dynamic parameters. In order to validate the numerical results, Experimental Modal Analysis of sandwich plate specimens was performed. Secondly, the double thickness wall is selected to be introduced in the RVE because of important error between numerical and experimental achievements. Comparative study validates the improved mechanical characteristics.

The knowledge of these constants is not sufficient and additional information about the delamination effects on the dynamical parameters of honeycomb composite panel is required. In present investigation this defect was implemented on the validated 3-D finite element model. The frequencies and associated modes shapes are obtained and analyzed.

Keywords

Article history

  1. ReceivedUntil the next stage: 28 days
  2. Revision requestedUntil the next stage: 8 days
  3. RevisedUntil the next stage: 17 days
  4. AcceptedUntil the next stage: 76 days
  5. Published

How to cite

APA

BENDADA, A., Boutchicha, D., Chouiter, A., & Miri, M. (2019). Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination. Fracture and Structural Integrity, 13(49), 655–665. https://doi.org/10.3221/IGF-ESIS.49.59

IEEE

A. BENDADA, D. Boutchicha, A. Chouiter, and M. Miri, “Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination,” Fracture and Structural Integrity, vol. 13, no. 49, pp. 655–665, 2019, doi: 10.3221/IGF-ESIS.49.59.

MLA

BENDADA, AYA, et al. “Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination.” Fracture and Structural Integrity, vol. 13, no. 49, 2019, pp. 655–665. https://doi.org/10.3221/IGF-ESIS.49.59.

Chicago

BENDADA, AYA, Djilali Boutchicha, Adel Chouiter, and Mokhtaria Miri. 2019. “Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination.” Fracture and Structural Integrity 13 (49): 655–665. https://doi.org/10.3221/IGF-ESIS.49.59.

Harvard

BENDADA, A., Boutchicha, D., Chouiter, A. and Miri, M. (2019) ‘Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination’, Fracture and Structural Integrity, 13(49), pp. 655–665. doi: 10.3221/IGF-ESIS.49.59.

Vancouver

BENDADA A, Boutchicha D, Chouiter A, Miri M. Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination. Fracture and Structural Integrity. 2019;13(49):655-665. doi:10.3221/IGF-ESIS.49.59

BibTeX

@article{bendada2019, author = {BENDADA, AYA and Boutchicha, Djilali and Chouiter, Adel and Miri, Mokhtaria}, title = {Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination}, journal = {Fracture and Structural Integrity}, year = {2019}, volume = {13}, number = {49}, pages = {655--665}, doi = {10.3221/IGF-ESIS.49.59}, url = {https://doi.org/10.3221/IGF-ESIS.49.59}, issn = {1971-8993} }

RIS

TY - JOUR AU - BENDADA, AYA AU - Boutchicha, Djilali AU - Chouiter, Adel AU - Miri, Mokhtaria TI - Numerical-Experimental characterization of honeycomb sandwich panel and numerical modal analysis of implemented delamination JO - Fracture and Structural Integrity T2 - Fracture and Structural Integrity PY - 2019 DA - 2019/06/22 VL - 13 IS - 49 SP - 655 EP - 665 DO - 10.3221/IGF-ESIS.49.59 UR - https://doi.org/10.3221/IGF-ESIS.49.59 SN - 1971-8993 ER -

Licence

Copyright © 2019 AYA BENDADA, Djilali Boutchicha, Adel Chouiter, Mokhtaria Miri.

Copyright 
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