Year 2024,
Volume: 02, 28 - 34, 31.07.2024
Merve Uslu
,
Mete Onur Kaman
,
Cenk Yanen
,
Mustafa Albayrak
,
Serkan Dağ
,
Serkan Erdem
,
Kadir Turan
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
Merve Uslu
,
Mete Onur Kaman
,
Cenk Yanen
,
Mustafa Albayrak
,
Serkan Dağ
,
Serkan Erdem
,
Kadir Turan
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)
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.