Taşyürek, MustafaÖdemiş, Okan2023-08-052023-08-052023 HazirTaşyürek, 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.12891452757-6574https://hdl.handle.net/20.500.12395/49172In 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.en10.55212/ijaa.1289145info:eu-repo/semantics/openAccessCarbon nanotubeLow speed impactNanocomposite reinforcementWood plate compositeArticle4118