Research Article
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Investigation of the effect of CNT reinforcement on low-velocity impact behavior of wooden plate honeycomb aircraft structures

Year 2023, Volume: 4 Issue: 1, 1 - 8, 30.06.2023
https://doi.org/10.55212/ijaa.1289145

Abstract

In this study, with different thicknesses honeycomb aircraft structures and the application of multi walled carbon nanotube reinforcement (MWCNT) to their out surfaces the low-velocity impact behavior of with the effects of core height on the damage to the plates were investigated. In addition, it is aimed to determine the effects of nano composite coating on the surface structure and to investigate its usability in aircraft. In the research, an equal to two different samples number of samples taken from the wing structure of the aerobatic aircraft, 10 and 30mm thick, 100x150mm in size, one surface coated with wood and the other surface covered with %1 carbon nanotube (CNT), were applied impact test at 5 J energy level and analyzed comparatively with graphics. The tests were carried out at an impact speed of 1.2549 m/s. Because of the research, it was concluded that while the reinforcement of CNT in aircraft structures did not affect the weight increase within the limitations, it gave positive results in the increase of strength without disturbing the aerodynamic structure and increased the mechanical properties. The data obtained from the force-time, force-displacement and energy-time changes obtained from the experiments are explained with the help of graphics.

References

  • Berkem, A., Ercan, H., Doğu, M. and Ünal, A. 2011. Investigation of Mechanical Behaviour of Honeycomb Composites Used in Aircraft Industry, 6th International Advanced Technologies Symposium (IATS’11), 16-18 May, Elazığ, Turkey, 475-480.
  • Akkuş, H. 2016. “Experimental and theoretical investigation of mechanical behaviors of honeycomb structures by using nano particle reinforced adhesive”. Ph.D. thesis, Selcuk University, Institute of Science and Technology, Mechanical Education Department, Konya, Turkey.
  • Aydın, S. 2019. Investigation of effects of carbon nanoparticles on epoxy adhesives, Çukurova University Journal of the Faculty of Engineering and Architecture, 34(3), 143-154.
  • Taşyürek, M., Ekinci, Ş. and Mirik, M. 2015. Investigation of mechanical properties of carbon nanotubes/high density polyethylene composites produced by extrusion method. Athens Journal of Technology & Engineering, 2(3), 181-192.
  • Rajoria, H. and Jalili, N. 2005. Passive vibration damping enhancement using carbon nanotube-epoxy reinforced composites. Composites Science and Technology, 65(14), 2079-2093.
  • Tarfaoui, M., Lafdi, K. and Moumen El, A. 2016. Mechanical properties of carbon nanotubes based polymer composites. Composites Part B: Engineering, 103(15), 113-121.
  • Zhengju, Z., Yanjie, H., Hao, J. and Chunzhong, Li. 2014. A Three-dimensional ordered mesoporous carbon/carbon nanotubes nanocomposites for supercapacitors. Journal of Power Sources, 246, 402-408.
  • Safadi, B., Andrews, R. and Grulke, E. A. 2002. Multiwalled carbon nanotube polymer composites: Synthesis and characterization of thin films. Journal of Applied Polymer Science, 84(14), 2660-2669.
  • Uyaner, M., Kara, M. and Ataberk, N. 2020. Size effect on low velocity impact behavior of laminatede-glass composite. Prooceedings of 8th International Fracture Conference, 7-9 November, İstanbul/Turkey, 361-368.
  • Esendemir, Ü. and Caner, A. Y. 2018. Experimental investigations on the impact behavior of laminated composite materials. Süleyman Demirel University, Journal of Natural and Applied Sciences, 22(1), 207-215.
  • Önal, T. and Temiz, Ş. 2021. Experimental investigation of impact behavior of balsa core sandwich composites. El-Cezerî Journal of Science and Engineering, 8(1), 333-345.
  • Erdoğan, Ö. 2020. “Low velocity impact behavior of sandwich panels”. M.Sc. thesis, Erciyes University, Graduate School of Natural and Applied Sciences, Kayseri, Turkey.
  • Taşyürek, M. and Kara M., 2018. Low-velocity ımpact response of pre-stressed grp tubes reinforced with carbon nanotubes. 4th ınternational conference on engineering and natural sciences (icens 2018), 2-6 May, Kiev, Ukraine, 601-606.
  • Taşyürek, M. and Tarakçioğlu, N. 2017. Enhancing fatigue life of filament winding laminar and curved pipes containing carbon nanotubes, and their fatıgue failure. Polymers & Polymer Composites, 25(2), 167-176.

CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi

Year 2023, Volume: 4 Issue: 1, 1 - 8, 30.06.2023
https://doi.org/10.55212/ijaa.1289145

Abstract

Bu çalışmada, farklı kalınlıklı ahşap plakalı bal peteği uçak yapıları ve bunların yüzeylerine çok duvarlı karbon nanotüp (MWCNT) takviye uygulamak suretiyle düşük hızlı darbe davranışlarının incelenmesi ile çekirdek yüksekliğinin plakalarda oluşan hasara etkileri incelenmiştir. Ayrıca nano kompozit kaplamanın yüzey yapısalı üzerine olan etkilerinin tespiti ile hava araçlarında kullanılabilirliğinin araştırılması da amaçlanmıştır. Araştırmada akrobasi uçağına ait kanat yapısalından alınan 10 ve 30mm kalınlıklı 100x150mm ebatlarında karşılıklı olarak bir yüzeyi ahşap diğer yüzeyi %1 oranında karbon nanotüp (CNT) ile kaplanmış eşit sayıdaki numunelere 5J enerji seviyesinde darbe testi uygulanmış ve karşılaştırmalı olarak grafiklerle analiz edilmiştir. Testler 1.2549 m/s çarpma hızında yapılmıştır. Araştırma neticesinde CNT uçak yapısallarında takviyelendirilme sinin ağırlık artışına sınırlamalar dâhilinde etki etmezken aerodinamik yapıyı bozmadan mukavemet artışında olumlu sonuçlar verdiği ve mekanik özellikleri arttırdığı sonucuna ulaşılmıştır. Deneylerden elde edilen kuvvet-zaman, kuvvet-deplasman ve enerji zaman değişimlerinden elde edilen veriler grafikler yardımıyla açıklanmıştır.

References

  • Berkem, A., Ercan, H., Doğu, M. and Ünal, A. 2011. Investigation of Mechanical Behaviour of Honeycomb Composites Used in Aircraft Industry, 6th International Advanced Technologies Symposium (IATS’11), 16-18 May, Elazığ, Turkey, 475-480.
  • Akkuş, H. 2016. “Experimental and theoretical investigation of mechanical behaviors of honeycomb structures by using nano particle reinforced adhesive”. Ph.D. thesis, Selcuk University, Institute of Science and Technology, Mechanical Education Department, Konya, Turkey.
  • Aydın, S. 2019. Investigation of effects of carbon nanoparticles on epoxy adhesives, Çukurova University Journal of the Faculty of Engineering and Architecture, 34(3), 143-154.
  • Taşyürek, M., Ekinci, Ş. and Mirik, M. 2015. Investigation of mechanical properties of carbon nanotubes/high density polyethylene composites produced by extrusion method. Athens Journal of Technology & Engineering, 2(3), 181-192.
  • Rajoria, H. and Jalili, N. 2005. Passive vibration damping enhancement using carbon nanotube-epoxy reinforced composites. Composites Science and Technology, 65(14), 2079-2093.
  • Tarfaoui, M., Lafdi, K. and Moumen El, A. 2016. Mechanical properties of carbon nanotubes based polymer composites. Composites Part B: Engineering, 103(15), 113-121.
  • Zhengju, Z., Yanjie, H., Hao, J. and Chunzhong, Li. 2014. A Three-dimensional ordered mesoporous carbon/carbon nanotubes nanocomposites for supercapacitors. Journal of Power Sources, 246, 402-408.
  • Safadi, B., Andrews, R. and Grulke, E. A. 2002. Multiwalled carbon nanotube polymer composites: Synthesis and characterization of thin films. Journal of Applied Polymer Science, 84(14), 2660-2669.
  • Uyaner, M., Kara, M. and Ataberk, N. 2020. Size effect on low velocity impact behavior of laminatede-glass composite. Prooceedings of 8th International Fracture Conference, 7-9 November, İstanbul/Turkey, 361-368.
  • Esendemir, Ü. and Caner, A. Y. 2018. Experimental investigations on the impact behavior of laminated composite materials. Süleyman Demirel University, Journal of Natural and Applied Sciences, 22(1), 207-215.
  • Önal, T. and Temiz, Ş. 2021. Experimental investigation of impact behavior of balsa core sandwich composites. El-Cezerî Journal of Science and Engineering, 8(1), 333-345.
  • Erdoğan, Ö. 2020. “Low velocity impact behavior of sandwich panels”. M.Sc. thesis, Erciyes University, Graduate School of Natural and Applied Sciences, Kayseri, Turkey.
  • Taşyürek, M. and Kara M., 2018. Low-velocity ımpact response of pre-stressed grp tubes reinforced with carbon nanotubes. 4th ınternational conference on engineering and natural sciences (icens 2018), 2-6 May, Kiev, Ukraine, 601-606.
  • Taşyürek, M. and Tarakçioğlu, N. 2017. Enhancing fatigue life of filament winding laminar and curved pipes containing carbon nanotubes, and their fatıgue failure. Polymers & Polymer Composites, 25(2), 167-176.
There are 14 citations in total.

Details

Primary Language Turkish
Subjects Aerospace Engineering
Journal Section Research Articles
Authors

Mustafa Taşyürek 0000-0001-9016-8584

Okan Ödemiş 0009-0006-1986-0184

Publication Date June 30, 2023
Submission Date April 28, 2023
Published in Issue Year 2023 Volume: 4 Issue: 1

Cite

APA Taşyürek, M., & Ödemiş, O. (2023). CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi. International Journal of Aeronautics and Astronautics, 4(1), 1-8. https://doi.org/10.55212/ijaa.1289145
AMA Taşyürek M, Ödemiş O. CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi. International Journal of Aeronautics and Astronautics. June 2023;4(1):1-8. doi:10.55212/ijaa.1289145
Chicago Taşyürek, Mustafa, and Okan Ödemiş. “CNT Takviyesinin ahşap Plakali Bal peteği uçak Yapilarinin düşük Hizli Darbe davranişlarina Etkisinin Incelenmesi”. International Journal of Aeronautics and Astronautics 4, no. 1 (June 2023): 1-8. https://doi.org/10.55212/ijaa.1289145.
EndNote Taşyürek M, Ödemiş O (June 1, 2023) CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi. International Journal of Aeronautics and Astronautics 4 1 1–8.
IEEE M. Taşyürek and O. Ödemiş, “CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi”, International Journal of Aeronautics and Astronautics, vol. 4, no. 1, pp. 1–8, 2023, doi: 10.55212/ijaa.1289145.
ISNAD Taşyürek, Mustafa - Ödemiş, Okan. “CNT Takviyesinin ahşap Plakali Bal peteği uçak Yapilarinin düşük Hizli Darbe davranişlarina Etkisinin Incelenmesi”. International Journal of Aeronautics and Astronautics 4/1 (June 2023), 1-8. https://doi.org/10.55212/ijaa.1289145.
JAMA Taşyürek M, Ödemiş O. CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi. International Journal of Aeronautics and Astronautics. 2023;4:1–8.
MLA Taşyürek, Mustafa and Okan Ödemiş. “CNT Takviyesinin ahşap Plakali Bal peteği uçak Yapilarinin düşük Hizli Darbe davranişlarina Etkisinin Incelenmesi”. International Journal of Aeronautics and Astronautics, vol. 4, no. 1, 2023, pp. 1-8, doi:10.55212/ijaa.1289145.
Vancouver Taşyürek M, Ödemiş O. CNT takviyesinin ahşap plakali bal peteği uçak yapilarinin düşük hizli darbe davranişlarina etkisinin incelenmesi. International Journal of Aeronautics and Astronautics. 2023;4(1):1-8.

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