Araştırma Makalesi
BibTex RIS Kaynak Göster
Yıl 2023, , 564 - 571, 30.06.2023
https://doi.org/10.16984/saufenbilder.1160160

Öz

Kaynakça

  • 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

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

Öz

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.

Kaynakça

  • 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.
Toplam 16 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Makine Mühendisliği
Bölüm Araştırma Makalesi
Yazarlar

Burak Şahin 0000-0002-8666-4902

Eyüp Yeter 0000-0002-0278-588X

Erken Görünüm Tarihi 22 Haziran 2023
Yayımlanma Tarihi 30 Haziran 2023
Gönderilme Tarihi 10 Ağustos 2022
Kabul Tarihi 4 Mart 2023
Yayımlandığı Sayı Yıl 2023

Kaynak Göster

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. Haziran 2023;27(3):564-571. doi:10.16984/saufenbilder.1160160
Chicago Şahin, Burak, ve Eyüp Yeter. “Lateral Buckling of Glare for Aerospace Application”. Sakarya University Journal of Science 27, sy. 3 (Haziran 2023): 564-71. https://doi.org/10.16984/saufenbilder.1160160.
EndNote Şahin B, Yeter E (01 Haziran 2023) Lateral Buckling of Glare for Aerospace Application. Sakarya University Journal of Science 27 3 564–571.
IEEE B. Şahin ve E. Yeter, “Lateral Buckling of Glare for Aerospace Application”, SAUJS, c. 27, sy. 3, ss. 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 (Haziran 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 ve Eyüp Yeter. “Lateral Buckling of Glare for Aerospace Application”. Sakarya University Journal of Science, c. 27, sy. 3, 2023, ss. 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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