Fracture and Structural Integrity e-ISSN 1971-8993 Open access
Advanced Manufacturing and Processing Vol. 13, No. 50 (2019)

The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel

Author and affiliation details
  • Ouadia Mouhat Corresponding author Mohammed V University, Structure LGCE l’EST, Salé -CED de l’EMI, Rabat, Morocco ouadie.mouhat@gmail.com
  • Abdelmajid Bybi Mohammed V University in Rabat, EST Sale - Morocco MEAT - Materials Energy Acoustics Team-CED of Mohammadia Engineering School, Rabat.
  • Ahmed El Bouhmidi Mohammed V University, Structure LGCE, EST Sale -CED of Mohammadia Engineering School, Rabat, Morocco.
  • Mohamed Rougui Mohammed V University, Structure LGCE, EST Sale -CED of Mohammadia Engineering School, Rabat, Morocco.
DOI
10.3221/IGF-ESIS.50.12
Pages
126-140
Published
Published inVol. 13, No. 50 (2019)Go to the issue

Abstract

In this paper, gradual demand for curved, stiffened panels composite emerged from carbon fiber reinforced plastics (CFRP); these are structures that are frequently used in aerospace engineering. Up to 50% of the primary structure of the Boeing 787 is made up of woven graphite–epoxy. This research emphasizes the buckling analysis of stiffened composite panels using the nonlinear, finite element modeling. The stiffened panel is assumed to be subjected to a uniform axial compression load of . For the nonlinear buckling analysis, a stiffened composite panel is made of carbon fibre composite (CFC) in epoxy, Kevlar in epoxy and E-glass (EG) in epoxy. Due to the fact that there are numerous stiffened composite panels materials, this paper, therefore uses a numerical approach, to present the study and results of the nonlinear static buckling analysis of I-stiffened, on different composite panels. This research also presented the effect of the different ply orientations using Abaqus finite element analysis (FEA).

Keywords

Article history

  1. ReceivedUntil the next stage: 27 days
  2. Revision requestedUntil the next stage: 10 days
  3. RevisedUntil the next stage: 0 days
  4. AcceptedUntil the next stage: 12 days
  5. Published

Statements

Funding

This work is sponsored by Structure LGCE ,EST Sale -CED of Mohammadia Engineering School Mohammed V University, Rabat

How to cite

APA

Mouhat, O., Bybi, A., El Bouhmidi, A., & Rougui, M. (2019). The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel. Fracture and Structural Integrity, 13(50), 126–140. https://doi.org/10.3221/IGF-ESIS.50.12

IEEE

O. Mouhat, A. Bybi, A. El Bouhmidi, and M. Rougui, “The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel,” Fracture and Structural Integrity, vol. 13, no. 50, pp. 126–140, 2019, doi: 10.3221/IGF-ESIS.50.12.

MLA

Mouhat, Ouadia, et al. “The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel.” Fracture and Structural Integrity, vol. 13, no. 50, 2019, pp. 126–140. https://doi.org/10.3221/IGF-ESIS.50.12.

Chicago

Mouhat, Ouadia, Abdelmajid Bybi, Ahmed El Bouhmidi, and Mohamed Rougui. 2019. “The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel.” Fracture and Structural Integrity 13 (50): 126–140. https://doi.org/10.3221/IGF-ESIS.50.12.

Harvard

Mouhat, O., Bybi, A., El Bouhmidi, A. and Rougui, M. (2019) ‘The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel’, Fracture and Structural Integrity, 13(50), pp. 126–140. doi: 10.3221/IGF-ESIS.50.12.

Vancouver

Mouhat O, Bybi A, El Bouhmidi A, Rougui M. The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel. Fracture and Structural Integrity. 2019;13(50):126-140. doi:10.3221/IGF-ESIS.50.12

BibTeX

@article{mouhat2019, author = {Mouhat, Ouadia and Bybi, Abdelmajid and El Bouhmidi, Ahmed and Rougui, Mohamed}, title = {The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel}, journal = {Fracture and Structural Integrity}, year = {2019}, volume = {13}, number = {50}, pages = {126--140}, doi = {10.3221/IGF-ESIS.50.12}, url = {https://doi.org/10.3221/IGF-ESIS.50.12}, issn = {1971-8993} }

RIS

TY - JOUR AU - Mouhat, Ouadia AU - Bybi, Abdelmajid AU - El Bouhmidi, Ahmed AU - Rougui, Mohamed TI - The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel JO - Fracture and Structural Integrity T2 - Fracture and Structural Integrity PY - 2019 DA - 2019/08/10 VL - 13 IS - 50 SP - 126 EP - 140 DO - 10.3221/IGF-ESIS.50.12 UR - https://doi.org/10.3221/IGF-ESIS.50.12 SN - 1971-8993 ER -

Licence

Copyright © 2019 Ouadia Mouhat, Abdelmajid Bybi, Ahmed El Bouhmidi, Mohamed Rougui.

Copyright 
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