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In this study, carbon fiber-reinforced plastic was used. (CFRP) stresses occurring in a disc have been studied by numerical analysis. The modulus of elasticity is constant with temperature, and the stresses occurring in the thermoplastic composite disc were studied by numerical analysis. Assuming that the modulus of elasticity does not change with temperature, the temperature distributions of 30°C, 60 °C, 90 °C, 120 °C, 150 °C were referenced in the study. CFRP materials are currently preferred in unmanned aerial vehicles, UAVs, SIHAS, aircraft industry. They are fiber-reinforced polymer materials obtained by combining carbon fibers with a polymer matrix, showing high strength, high hardness and strength. The stress values obtained at the end of the study were compared among themselves and shared with the literature in graphs. It was concluded that an increase in the value of the temperature acting on the CFRP disc correctly affects thermal stresses. At the same time, the results obtained were analyzed with the ANYS 2023 finite element program. It has been seen that the results obtained are compatible with each other.
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Birincil Dil | İngilizce |
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Konular | İnşaat Mühendisliğinde Sayısal Modelleme, Yapım Teknolojileri |
Bölüm | Araştırma Makalesi |
Yazarlar | |
Proje Numarası | _ |
Yayımlanma Tarihi | 25 Ocak 2024 |
Gönderilme Tarihi | 9 Ocak 2024 |
Kabul Tarihi | 22 Ocak 2024 |
Yayımlandığı Sayı | Yıl 2024 Cilt: 01 |