Investigation of the Effect of CNT Reinforcement on Low-Velocity Impact Behavior of Wooden Plate Honeycomb Aircraft Structures

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dc.authorid0000-0001-9016-8584en_US
dc.authorid0009-0006-1986-0184en_US
dc.contributor.authorTaşyürek, Mustafa
dc.contributor.authorÖdemiş, Okan
dc.date.accessioned2023-08-05T08:46:45Z
dc.date.available2023-08-05T08:46:45Z
dc.date.issued2023 Haziranen_US
dc.departmentSelçuk Üniversitesi, Yüksek Okullar, Sivil Havacılık Yüksekokuluen_US
dc.description.abstractIn 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.en_US
dc.identifier.citationTaşyürek, 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.1289145en_US
dc.identifier.doi10.55212/ijaa.1289145en_US
dc.identifier.endpage8en_US
dc.identifier.issn2757-6574en_US
dc.identifier.issue1en_US
dc.identifier.startpage1en_US
dc.identifier.urihttps://hdl.handle.net/20.500.12395/49172
dc.identifier.volume4en_US
dc.institutionauthorTaşyürek, Mustafa
dc.institutionauthorÖdemiş, Okan
dc.language.isoenen_US
dc.publisherSelçuk Üniversitesien_US
dc.relation.ispartofInternational Journal of Aeronautics and Astronauticsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.selcuk20240510_oaigen_US
dc.subjectCarbon nanotubeen_US
dc.subjectLow speed impacten_US
dc.subjectNanocomposite reinforcementen_US
dc.subjectWood plate compositeen_US
dc.titleInvestigation of the Effect of CNT Reinforcement on Low-Velocity Impact Behavior of Wooden Plate Honeycomb Aircraft Structuresen_US
dc.typeArticleen_US

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