STRUCTURE ANALYSIS AND MANUFACTURING OF WINGS TRAINER-5774

Abstract

Unmanned Aerial Vechicle (UAV) is one of the types an aircraft. Trainer is part of an airplane where the aircraft is controlled by a remote control for its flight. One of the things that must be considred in design an airplane is strength and and resistance of the wing structure in accepting distributed aircraft loads. In addition to the structural design and load, the material to be used can have an effect. The process is starting from modification of the aircraft wing using CATIA V5R20 which is then carried out analysis of the wing structure by being given the aircraft load using ANSYS 19. The largest structural value is in the Joiner section of 7,967 with manuvering load and smallest value is 0,026 on the Spar section. Margin of safety smallest value in the spar when its manuver. After analysis it is continued with the manufacturing process according to the design that has been made.

Keywords

Trainer-5774; analisis sruktur; margin of safety; load factor

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References

Astasari.2017. Pengaruh Variasi Arah Serat Dan Jumlah Layer Terhadap Karakteristik Bending Dan Torsional Stiffness Komposit Sandwich Serat Karbon Dengan Core Kayu Balsa, Institut Teknologi Sepuluh November, Surabaya. Civil Aviation Safety Authority Australia, (2000). Design Standards: Unmanned Aerial Vehicles – Aeroplanes. 2000. Gibson, Ronald F.1994. Principle Of Composite Material Mechanics.United States of America, Amerika. Kurniawan. M . H, 2017. Analisis Kekuatan Wing Pesawat UAV MAC 01 Terhadap Bending Dan Torsi, Sekolah Tinggi Teknologi Adisutjipto, Yogyakarta. Martin, J . W. 2006. Materials For Engineering, Boca Raton Boston New York Washington, DC. Mohammadi, Meisam Shir dan Nairn,John A. 2014. Crack propagation and fracture toughness of solid balsa used for cores of sandwich composites, Oregon State University, USA. Mokhtar, M., Rahmat, A . R., Hassan, A. 2007. Characterization And Treatments of Pineapple Thermoplastic Composite For Construction Application. Universitas Teknologi Malaysia, Malaysia. [8] Niu, Michael Chun-yung. 1998. Airframe Structural Design. Conmilit Press Ltd, California. Pecas, P., Cavalho, H., Salman H., Leite, M. 2018. Journal of Composite Science, Portugal. Purboningrum, S.C.2020. Modifikasi Dan Manufaktur Batang Vtol ( Vertical Take Off Landing ) Pesawat UAV V-Sky STTA, Sekolah Tinggi Teknologi Adisutjipto, Yogyakarta. Saputra, W . E. 2019. Modifikasi UAV V-SKY 14 Dan Analisis Kekuatan Struktur Sayap, Fuselage, Dan Tail UAV V-SKY 14 NG Menggunkan Software MSC Patran/Nastran, Sekolah Tinggi Teknologi Adisutjipto, Yogyakarta.

http://dx.doi.org/10.28989/vortex.v1i2.894

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