Investigation of the Effect of CNT Reinforcement on Low-Velocity Impact Behavior of Wooden Plate Honeycomb Aircraft Structures
Yükleniyor...
Dosyalar
Tarih
2023 Haziran
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Selçuk Üniversitesi
Erişim Hakkı
info:eu-repo/semantics/openAccess
Özet
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.
Açıklama
Anahtar Kelimeler
Carbon nanotube, Low speed impact, Nanocomposite reinforcement, Wood plate composite
Kaynak
International Journal of Aeronautics and Astronautics
WoS Q Değeri
Scopus Q Değeri
Cilt
4
Sayı
1
Künye
Taşyürek, M., Ödemiş, O., (2023). Investigation of the Effect of CNT Reinforcement on Low-Velocity Impact Behavior of Wooden Plate Honeycomb Aircraft Structures. International Journal of Aeronautics and Astronautics, 4(1), 1-8.
DOI: 10.55212/ijaa.1289145
