Research Article
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Year 2023, , 564 - 571, 30.06.2023
https://doi.org/10.16984/saufenbilder.1160160

Abstract

References

  • K. H. Rendigs, M. Knüwer, “Metal materials in Airbus 380,” 2nd Izmir Global Aerospace & Offset Conference, October 6−8, 2010, Izmir.
  • D. Banat, R. J. Mania, R. Degenhardt, “Stress state failure analysis of thin-walled GLARE composite members subjected to axial loading in the post-buckling range,” Composite Structures, vol 289, pp. 1-11, 2022.
  • G. Wu, J. M. Yang, “The Mechanical Behavior of GLARE Laminates for Aircraft Structures,” Failure in Structural Materials, pp. 72-79, 2005.
  • T. Sinmazçelik, E. Avcu, M.Ö. Bora, O. Çoban, “A review: Fibre metal laminates, background, bonding types and applied test methods,” Materials and Design vol 32, pp. 3671–3685, 2011.
  • A. S. M. Al-Azzawi, J. McCrory, L. F. Kawashita, C. A. Featherston, R. Pullin, K. M. Holford, “Buckling and postbuckling behaviour of Glare laminates containing splices and doublers. Part 1: Instrumented tests,” Composite Structures, vol 176 pp. 1158–1169, 2017.
  • R. J. Mania, C. BronnYork “Buckling strength improvements for Fibre Metal Laminates using thin-ply tailoring,” Composite Structures vol 159, pp. 424–432, 2017.
  • D. Banat, R. J. Mania, “Stability and strength analysis of thin-walled GLARE composite profiles subjected to axial loading,” Composite Structures, vol 212, pp. 338–345, 2019.
  • E. Eglitis, K. Kalnins, O. Ozolinsh, “The influence of loading eccentricity on the buckling of axially compressed imperfect composite cylinders,” Mechanics of Composite Materials, vol 46, no 5, pp. 83–92, 2010.
  • G. S. E. Bikakis, C. D. Kalfountzos, E. E. Theotokoglou, “Elastic buckling response of rectangular GLARE fiber-metal laminates subjected to shearing stresses,” Aerospace Science and Technology, vol 87, pp. 110–118, 2019.
  • P. P. Y. Muddappa, G. Giridhara, T. Rajanna, “Buckling behavior of GLARE panels subjected to partial edge loads,” Materials Today: Proceedings, vol 45, pp. 94–99, 2021.
  • D. Banat, Z. Kolakowski, R. J. Mania, “Investigations of fml profile buckling and post-buckling behaviour under axial compression,” Thin-Walled Structures, vol 107, pp. 335–344, 2016.
  • L. B. Vogelesang, A. Vlot, “Development of fibre metal laminates for advanced aerospace structures,” Journal of Materials Processing Technology, vol 103, pp. 1-5, 2000.
  • A. Erklig, E. Yeter, M. Bulut, “The effects of cut-outs on lateral buckling behavior of laminated composite beams,” Composite Structures, vol 104, pp. 54–59, 2013.
  • A. Erklig, E. Yeter, “The effects of cutouts on buckling behavior of composite plates,” Sci Eng Compos Mater, vol 19, pp. 323-330, 2012.
  • E. Yeter, A. Erklig, M. Bulut, “Hybridization effects on lateral buckling behavior of laminated composite beams,” Polymer Composites, vol 37 issue8, pp. 2511, 2521, 2016.
  • A. Erklig, E. Yeter,, “Kompozit Malzemelere Açılan Dairesel, Kare, Üçgen ve Eliptik Kesitlerin Burkulmaya Etkisinin Sonlu Eleman Yöntemiyle Araştırılması”, Theoretical and Applied Mechanical Turkish National Committee, 2011.

Lateral Buckling of Glare for Aerospace Application

Year 2023, , 564 - 571, 30.06.2023
https://doi.org/10.16984/saufenbilder.1160160

Abstract

Glare (Glass Reinforced Aluminium) which consists of fibre metal laminate composite consisting of aluminium and glass is used aerospace structures are supposed to buckling and impact loads. Lateral buckling analyses were made to determine critical buckling loads, and results were compared to Al 2024-T3 in this paper. Weight and load carrying capacity of Glare grades were taken into consideration and the importance of weight to critical load was stated. Numerical works were carried out by starting with Glass and Aluminum then continued for Glare Grades of Glare 2A, Glare 2B, Glare 3A, Glare 3B, Glare 4A, Glare 4B, Glare 5A, Glare 5B, Glare 6A and Glare 6B to estimate buckling load values. Several comparisons were presented for Glare grades based on Al 2024-T3 through paper. Glare 2A, 2B, 3A, 3B, 6A and 6B Grades have lower weight and buckling load values compared to Al 2024-T3. Lower weight is essential for aerospace applications. But optimum weight and load carrying capacity can be selected for intended applications by taking weight and load into consideration at same time. Although Glare grades of 4A 2-1, 4B 2-1, 5A 2-1 and 5B 2-1 having closer weight (17.60g, 17.60g, 19.13g and 19.13g respectively) to Al 2024-T3 (17.31g), higher buckling loads were determined for Glare grades numerically. The best choice for Glare as an alternative to Al 2024-T3 under lateral buckling loading can be decided for point of views of less weight to critical load ratio.

References

  • K. H. Rendigs, M. Knüwer, “Metal materials in Airbus 380,” 2nd Izmir Global Aerospace & Offset Conference, October 6−8, 2010, Izmir.
  • D. Banat, R. J. Mania, R. Degenhardt, “Stress state failure analysis of thin-walled GLARE composite members subjected to axial loading in the post-buckling range,” Composite Structures, vol 289, pp. 1-11, 2022.
  • G. Wu, J. M. Yang, “The Mechanical Behavior of GLARE Laminates for Aircraft Structures,” Failure in Structural Materials, pp. 72-79, 2005.
  • T. Sinmazçelik, E. Avcu, M.Ö. Bora, O. Çoban, “A review: Fibre metal laminates, background, bonding types and applied test methods,” Materials and Design vol 32, pp. 3671–3685, 2011.
  • A. S. M. Al-Azzawi, J. McCrory, L. F. Kawashita, C. A. Featherston, R. Pullin, K. M. Holford, “Buckling and postbuckling behaviour of Glare laminates containing splices and doublers. Part 1: Instrumented tests,” Composite Structures, vol 176 pp. 1158–1169, 2017.
  • R. J. Mania, C. BronnYork “Buckling strength improvements for Fibre Metal Laminates using thin-ply tailoring,” Composite Structures vol 159, pp. 424–432, 2017.
  • D. Banat, R. J. Mania, “Stability and strength analysis of thin-walled GLARE composite profiles subjected to axial loading,” Composite Structures, vol 212, pp. 338–345, 2019.
  • E. Eglitis, K. Kalnins, O. Ozolinsh, “The influence of loading eccentricity on the buckling of axially compressed imperfect composite cylinders,” Mechanics of Composite Materials, vol 46, no 5, pp. 83–92, 2010.
  • G. S. E. Bikakis, C. D. Kalfountzos, E. E. Theotokoglou, “Elastic buckling response of rectangular GLARE fiber-metal laminates subjected to shearing stresses,” Aerospace Science and Technology, vol 87, pp. 110–118, 2019.
  • P. P. Y. Muddappa, G. Giridhara, T. Rajanna, “Buckling behavior of GLARE panels subjected to partial edge loads,” Materials Today: Proceedings, vol 45, pp. 94–99, 2021.
  • D. Banat, Z. Kolakowski, R. J. Mania, “Investigations of fml profile buckling and post-buckling behaviour under axial compression,” Thin-Walled Structures, vol 107, pp. 335–344, 2016.
  • L. B. Vogelesang, A. Vlot, “Development of fibre metal laminates for advanced aerospace structures,” Journal of Materials Processing Technology, vol 103, pp. 1-5, 2000.
  • A. Erklig, E. Yeter, M. Bulut, “The effects of cut-outs on lateral buckling behavior of laminated composite beams,” Composite Structures, vol 104, pp. 54–59, 2013.
  • A. Erklig, E. Yeter, “The effects of cutouts on buckling behavior of composite plates,” Sci Eng Compos Mater, vol 19, pp. 323-330, 2012.
  • E. Yeter, A. Erklig, M. Bulut, “Hybridization effects on lateral buckling behavior of laminated composite beams,” Polymer Composites, vol 37 issue8, pp. 2511, 2521, 2016.
  • A. Erklig, E. Yeter,, “Kompozit Malzemelere Açılan Dairesel, Kare, Üçgen ve Eliptik Kesitlerin Burkulmaya Etkisinin Sonlu Eleman Yöntemiyle Araştırılması”, Theoretical and Applied Mechanical Turkish National Committee, 2011.
There are 16 citations in total.

Details

Primary Language English
Subjects Mechanical Engineering
Journal Section Research Articles
Authors

Burak Şahin 0000-0002-8666-4902

Eyüp Yeter 0000-0002-0278-588X

Early Pub Date June 22, 2023
Publication Date June 30, 2023
Submission Date August 10, 2022
Acceptance Date March 4, 2023
Published in Issue Year 2023

Cite

APA Şahin, B., & Yeter, E. (2023). Lateral Buckling of Glare for Aerospace Application. Sakarya University Journal of Science, 27(3), 564-571. https://doi.org/10.16984/saufenbilder.1160160
AMA Şahin B, Yeter E. Lateral Buckling of Glare for Aerospace Application. SAUJS. June 2023;27(3):564-571. doi:10.16984/saufenbilder.1160160
Chicago Şahin, Burak, and Eyüp Yeter. “Lateral Buckling of Glare for Aerospace Application”. Sakarya University Journal of Science 27, no. 3 (June 2023): 564-71. https://doi.org/10.16984/saufenbilder.1160160.
EndNote Şahin B, Yeter E (June 1, 2023) Lateral Buckling of Glare for Aerospace Application. Sakarya University Journal of Science 27 3 564–571.
IEEE B. Şahin and E. Yeter, “Lateral Buckling of Glare for Aerospace Application”, SAUJS, vol. 27, no. 3, pp. 564–571, 2023, doi: 10.16984/saufenbilder.1160160.
ISNAD Şahin, Burak - Yeter, Eyüp. “Lateral Buckling of Glare for Aerospace Application”. Sakarya University Journal of Science 27/3 (June 2023), 564-571. https://doi.org/10.16984/saufenbilder.1160160.
JAMA Şahin B, Yeter E. Lateral Buckling of Glare for Aerospace Application. SAUJS. 2023;27:564–571.
MLA Şahin, Burak and Eyüp Yeter. “Lateral Buckling of Glare for Aerospace Application”. Sakarya University Journal of Science, vol. 27, no. 3, 2023, pp. 564-71, doi:10.16984/saufenbilder.1160160.
Vancouver Şahin B, Yeter E. Lateral Buckling of Glare for Aerospace Application. SAUJS. 2023;27(3):564-71.

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