Research Article
BibTex RIS Cite
Year 2024, Volume: 02, 28 - 34, 31.07.2024

Abstract

Project Number

123M357

References

  • F. Elaldi and L. Colak, “Buckling and Post-buckling Behavior of Compression Loaded Composite Panels with Hat Stiffeners,” J. Reinf. Plast. Compos., vol. 28, no. 20, pp. 2501–2509, Sep. 2008, doi: 10.1177/0731684408092394.
  • 2. Y. Feng, H. Zhang, X. Tan, Y. He, T. An, and J. Zheng, “Effect of impact damage positions on the buckling and post-buckling behaviors of stiffened composite panel,” Compos. Struct., vol. 155, pp. 184–196, 2016, doi: https://doi.org/10.1016/j.compstruct.2016.08.012.
  • 3. A. Kurşun, M. Şenel, H. M. Enginsoy, and E. Bayraktar, “Effect of impactor shapes on the low velocity impact damage of sandwich composite plate: Experimental study and modelling,” Compos. Part B Eng., vol. 86, pp. 143–151, 2016, doi: https://doi.org/10.1016/j.compositesb.2015.09.032.
  • 4. X. Han, S. Hou, L. Ying, W. Hou, and H. Aliyev, “On the fracture behaviour of adhesively bonded CFRP hat-shaped thin-walled beam under axial crushing load: An experimental and modelling study,” Compos. Struct., vol. 215, pp. 258–265, 2019, doi: https://doi.org/10.1016/j.compstruct.2019.01.075.
  • 5. F. Alkhatib, E. Mahdi, and A. Dean, “Crushing response of CFRP and KFRP composite corrugated tubes to quasi-static slipping axial loading: Experimental investigation and numerical simulation,” Compos. Struct., vol. 246, p. 112370, 2020, doi: https://doi.org/10.1016/j.compstruct.2020.112370.
  • 6. S. Kumar, R. Kumar, and S. Mandal, “Experimental and FE analysis for the buckling behavior of hat-stiffened panels under edge compressive loading,” Sādhanā, vol. 45, no. 1, p. 130, 2020, doi: 10.1007/s12046-020-01364-8.
  • 7. Z. Sun et al., “Prediction of compression buckling load and buckling mode of hat-stiffened panels using artificial neural network,” Eng. Struct., vol. 242, p. 112275, 2021, doi: https://doi.org/10.1016/j.engstruct.2021.112275.
  • 8. P. B. Ataabadi, D. Karagiozova, and M. Alves, “Finite element modeling of crushing of CFRP cylindrical tubes under low-velocity axial impact,” Compos. Struct., vol. 280, p. 114902, 2022, doi: https://doi.org/10.1016/j.compstruct.2021.114902.
  • 9. Y. Feng, S. Liu, T. Zhang, and S. Jiao, “Experimental and theoretical investigation on the shear performance of stiffened composite panel with I-shaped stiffeners,” Compos. Struct., vol. 284, p. 115234, 2022, doi: https://doi.org/10.1016/j.compstruct.2022.115234.
  • 10. B. Li, Y. Gong, Y. Gao, M. Hou, and L. Li, “Failure Analysis of Hat-Stringer-Stiffened Aircraft Composite Panels under Four-Point Bending Loading,” Materials, vol. 15, no. 7. 2022. doi: 10.3390/ma15072430.
  • 11. L. Liu and W. Xu, “Effects of fillers on the impact damage and compressive residual properties of single hat-stiffened composite panels,” Thin-Walled Struct., vol. 180, p. 109705, 2022, doi: https://doi.org/10.1016/j.tws.2022.109705.
  • 12. Y. Hou, J. Huang, Y. Liu, L. Meng, T. Sapanathan, and Y. Xu, “Low-velocity impact and compression after impact behaviors of rib-stiffened CFRP panels: Experimental and numerical study,” Aerosp. Sci. Technol., vol. 146, p. 108948, 2024, doi: https://doi.org/10.1016/j.ast.2024.108948.
  • 13. A. P. Kumar, J. P. Mendez, R. G. Burela, C. Bisagni, D. Harursampath and S. A. Ponnusami, “Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method,” Compos. Struct, vol. 345, p. 118276, 2024, doi: https://doi.org/10.1016/j.compstruct.2024.118276.
  • 14. Ahmadi H., Rahimi G., “Analytical and experimental investigation of transverse loading on grid stiffened composite panels”, Composites B, v. 159 2019,p.184-198, doi:https://doi.org/10.1016/j.compstruct.2022.116339.
  • 15. Wu Q., Hu S., Tang X., Liu X., Chen Z., Xiong J., “Compressive buckling and post-buckling behaviors of J-type composite stiffened panel before and after impact load,” Compos Struct, v. 304, 2023, p. 116339, doi: https://doi.org/10.1016/j.compstruct.2022.116339.
  • 16. Suriani M., Rapi H.Z., Ilyas R., Petru M., Sapuan S. “Delamination and manufacturing defects in natural fiber-reinforced hybrid composite: A review”, Polymers, v.13, no. 8, 2021, p. 1323 doi: https://doi.org/10.3390/polym13081323.
  • 17. Kong X., Yang Y., Gan J., Yuan T., Ao L., Wu, “Experimental and numerical investigation on the detailed buckling process of similar stiffened panels subjected to in-plane compressive load”,Thin-Walled Struct, v.148, 2020, p. 106620, doi: https://doi.org/10.1016/j.tws.2020.106620.
  • 18. Kolanu N.R., Raju G., Ramji, “Experimental and numerical studies on the buckling and post-buckling behavior of single blade-stiffened CFRP panels”, Compos Struct, v.196, 2018, p. 135-154, doi: https://doi.org/10.1016/j.compstruct.2018.05.015.
  • 19. van Dooren K.S., Tijs B., Waleson J., Bisagni C., “Skin-stringer separation in post-buckling of butt-joint stiffened thermoplastic composite panels”, Compos Struct, v.304, 2023, p. 116294, doi: https://doi.org/10.1016/j.compstruct.2022.116294.
  • 20. Albayrak, M., Kaman, MO, Bozkurt, I., “Kauçuk Ara Katmanlı Kavisli Kompozitler İçin Düşük Hızlı Darbe Davranışı Üzerindeki Geometrik Etkinin Den-eysel ve Sayısal Araştırması.” Appl Compos Ma-ter,v.30 , p.507–538, 2023. doi:https://doi.org/10.1007/s10443-022-10094-5
  • 21. Erdem, S., Kaman MO.,Gür M., "Karbon fiber epoksi kompozit levhaların burkulma sonrası dav-ranışı." Mekanik Bilim ve Teknoloji Dergisi, v.33, 2019, p.1723-1730.
  • 22. Bozkurt, I., Kaman, MO, Albayrak, M., “Farklı hücre tipleri için tamamen karbon fiber kompozitten üretilen sandviçlerin düşük hızlı darbe davranışları ve farklı çekirdek tipleri için sıkıştırma dav-ranışları.” Malzeme Testleri, v.65, no.9, p.1349-1372.

Design and production of new type reinforced U-profile composite panels

Year 2024, Volume: 02, 28 - 34, 31.07.2024

Abstract

In aircraft design, factors such as fuel efficiency, lightness and durability are critical due to the effect of various loads. Therefore, the use of "U" profile beams, which are stronger in terms of strength, provides versatile advantages. In this study, a reinforced composite panel was designed and fabricated by adding support beams to the "U" profiles to maintain the safety and integrity of aircraft structures. Glass fiber and epoxy resin were employed in the composite production process. The vacuum infusion method was employed for composite production, with molds specifically designed for the "U" profile and "I" support beams. Following production, the compatibility of the "U" profile, "I" support beam and sub-composite base forming the composite panel was evaluated. It was determined that the produced "I" support beam constituted only 18.8% by weight of the composite panel.

Supporting Institution

Scientific and Technological Research Council of Turkey (TUBITAK)

Project Number

123M357

Thanks

This study was supported by Scientific and Technological Research Council of Turkey (TUBITAK) under the Grant Number 123M357. The authors thank to TUBITAK for their supports.

References

  • F. Elaldi and L. Colak, “Buckling and Post-buckling Behavior of Compression Loaded Composite Panels with Hat Stiffeners,” J. Reinf. Plast. Compos., vol. 28, no. 20, pp. 2501–2509, Sep. 2008, doi: 10.1177/0731684408092394.
  • 2. Y. Feng, H. Zhang, X. Tan, Y. He, T. An, and J. Zheng, “Effect of impact damage positions on the buckling and post-buckling behaviors of stiffened composite panel,” Compos. Struct., vol. 155, pp. 184–196, 2016, doi: https://doi.org/10.1016/j.compstruct.2016.08.012.
  • 3. A. Kurşun, M. Şenel, H. M. Enginsoy, and E. Bayraktar, “Effect of impactor shapes on the low velocity impact damage of sandwich composite plate: Experimental study and modelling,” Compos. Part B Eng., vol. 86, pp. 143–151, 2016, doi: https://doi.org/10.1016/j.compositesb.2015.09.032.
  • 4. X. Han, S. Hou, L. Ying, W. Hou, and H. Aliyev, “On the fracture behaviour of adhesively bonded CFRP hat-shaped thin-walled beam under axial crushing load: An experimental and modelling study,” Compos. Struct., vol. 215, pp. 258–265, 2019, doi: https://doi.org/10.1016/j.compstruct.2019.01.075.
  • 5. F. Alkhatib, E. Mahdi, and A. Dean, “Crushing response of CFRP and KFRP composite corrugated tubes to quasi-static slipping axial loading: Experimental investigation and numerical simulation,” Compos. Struct., vol. 246, p. 112370, 2020, doi: https://doi.org/10.1016/j.compstruct.2020.112370.
  • 6. S. Kumar, R. Kumar, and S. Mandal, “Experimental and FE analysis for the buckling behavior of hat-stiffened panels under edge compressive loading,” Sādhanā, vol. 45, no. 1, p. 130, 2020, doi: 10.1007/s12046-020-01364-8.
  • 7. Z. Sun et al., “Prediction of compression buckling load and buckling mode of hat-stiffened panels using artificial neural network,” Eng. Struct., vol. 242, p. 112275, 2021, doi: https://doi.org/10.1016/j.engstruct.2021.112275.
  • 8. P. B. Ataabadi, D. Karagiozova, and M. Alves, “Finite element modeling of crushing of CFRP cylindrical tubes under low-velocity axial impact,” Compos. Struct., vol. 280, p. 114902, 2022, doi: https://doi.org/10.1016/j.compstruct.2021.114902.
  • 9. Y. Feng, S. Liu, T. Zhang, and S. Jiao, “Experimental and theoretical investigation on the shear performance of stiffened composite panel with I-shaped stiffeners,” Compos. Struct., vol. 284, p. 115234, 2022, doi: https://doi.org/10.1016/j.compstruct.2022.115234.
  • 10. B. Li, Y. Gong, Y. Gao, M. Hou, and L. Li, “Failure Analysis of Hat-Stringer-Stiffened Aircraft Composite Panels under Four-Point Bending Loading,” Materials, vol. 15, no. 7. 2022. doi: 10.3390/ma15072430.
  • 11. L. Liu and W. Xu, “Effects of fillers on the impact damage and compressive residual properties of single hat-stiffened composite panels,” Thin-Walled Struct., vol. 180, p. 109705, 2022, doi: https://doi.org/10.1016/j.tws.2022.109705.
  • 12. Y. Hou, J. Huang, Y. Liu, L. Meng, T. Sapanathan, and Y. Xu, “Low-velocity impact and compression after impact behaviors of rib-stiffened CFRP panels: Experimental and numerical study,” Aerosp. Sci. Technol., vol. 146, p. 108948, 2024, doi: https://doi.org/10.1016/j.ast.2024.108948.
  • 13. A. P. Kumar, J. P. Mendez, R. G. Burela, C. Bisagni, D. Harursampath and S. A. Ponnusami, “Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method,” Compos. Struct, vol. 345, p. 118276, 2024, doi: https://doi.org/10.1016/j.compstruct.2024.118276.
  • 14. Ahmadi H., Rahimi G., “Analytical and experimental investigation of transverse loading on grid stiffened composite panels”, Composites B, v. 159 2019,p.184-198, doi:https://doi.org/10.1016/j.compstruct.2022.116339.
  • 15. Wu Q., Hu S., Tang X., Liu X., Chen Z., Xiong J., “Compressive buckling and post-buckling behaviors of J-type composite stiffened panel before and after impact load,” Compos Struct, v. 304, 2023, p. 116339, doi: https://doi.org/10.1016/j.compstruct.2022.116339.
  • 16. Suriani M., Rapi H.Z., Ilyas R., Petru M., Sapuan S. “Delamination and manufacturing defects in natural fiber-reinforced hybrid composite: A review”, Polymers, v.13, no. 8, 2021, p. 1323 doi: https://doi.org/10.3390/polym13081323.
  • 17. Kong X., Yang Y., Gan J., Yuan T., Ao L., Wu, “Experimental and numerical investigation on the detailed buckling process of similar stiffened panels subjected to in-plane compressive load”,Thin-Walled Struct, v.148, 2020, p. 106620, doi: https://doi.org/10.1016/j.tws.2020.106620.
  • 18. Kolanu N.R., Raju G., Ramji, “Experimental and numerical studies on the buckling and post-buckling behavior of single blade-stiffened CFRP panels”, Compos Struct, v.196, 2018, p. 135-154, doi: https://doi.org/10.1016/j.compstruct.2018.05.015.
  • 19. van Dooren K.S., Tijs B., Waleson J., Bisagni C., “Skin-stringer separation in post-buckling of butt-joint stiffened thermoplastic composite panels”, Compos Struct, v.304, 2023, p. 116294, doi: https://doi.org/10.1016/j.compstruct.2022.116294.
  • 20. Albayrak, M., Kaman, MO, Bozkurt, I., “Kauçuk Ara Katmanlı Kavisli Kompozitler İçin Düşük Hızlı Darbe Davranışı Üzerindeki Geometrik Etkinin Den-eysel ve Sayısal Araştırması.” Appl Compos Ma-ter,v.30 , p.507–538, 2023. doi:https://doi.org/10.1007/s10443-022-10094-5
  • 21. Erdem, S., Kaman MO.,Gür M., "Karbon fiber epoksi kompozit levhaların burkulma sonrası dav-ranışı." Mekanik Bilim ve Teknoloji Dergisi, v.33, 2019, p.1723-1730.
  • 22. Bozkurt, I., Kaman, MO, Albayrak, M., “Farklı hücre tipleri için tamamen karbon fiber kompozitten üretilen sandviçlerin düşük hızlı darbe davranışları ve farklı çekirdek tipleri için sıkıştırma dav-ranışları.” Malzeme Testleri, v.65, no.9, p.1349-1372.
There are 22 citations in total.

Details

Primary Language English
Subjects Solid Mechanics, Material Design and Behaviors
Journal Section Research Articles
Authors

Merve Uslu

Mete Onur Kaman

Cenk Yanen 0000-0002-5092-8734

Mustafa Albayrak 0000-0002-2913-6652

Serkan Dağ

Serkan Erdem

Kadir Turan 0000-0002-4065-9649

Project Number 123M357
Publication Date July 31, 2024
Submission Date June 28, 2024
Acceptance Date July 27, 2024
Published in Issue Year 2024 Volume: 02

Cite

Vancouver Uslu M, Kaman MO, Yanen C, Albayrak M, Dağ S, Erdem S, Turan K. Design and production of new type reinforced U-profile composite panels. JOEBS. 2024;02:28-34.



Google Scholar                            Academic Resource Index                         Creative Commons Attribution 4.0 International License