Lasinta Ari Nendra Wibawa (2020) Simulasi Umur Fatik Rangka Main Landing Gear Menggunakan Metode Elemen Hingga. Dinamika dan Teknik Mesin : Jurnal Keilmuan dan Terapan Teknik Mesin, 10 (2). pp. 120-126. ISSN 2088-008X
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Abstract
The landing gear is one crucial component in an Unmanned Aerial Vehicle (UAV) aircraft construction. Landing gear serves as the main supporting component of aircraft load when landing and take off. This research aims to investigate the fatigue design life of the main landing gear on the UAV aircraft. The main landing gear frame design used Autodesk Inventor Professional 2017, while finite element analysis used Ansys Workbench software. It is subjected to a load of 1500 N with a loading fully-reserved. The prediction for fatigue life using Gerber mean stress theory. The material of the main landing gear frame is Aluminum alloy 6061. The simulation results show that the main landing gear frame has a minimum fatigue life of up to 3.5 x 107 cycles with a minimum safety factor of 1.43.
| Item Type: | Article |
|---|---|
| Additional Information: | judul dalam bahasa Inggris : Fatigue Life Simulation of Main Landing Gear Frame using The Finite Element Method |
| Uncontrolled Keywords: | Main landing gear, Unmanned aerial vehicle, Fatigue life, Finite element method Ansys |
| Subjects: | Taksonomi LAPAN > Teknologi Penerbangan dan Antariksa > Penelitian, Pengembangan, Perekayasaan, dan Pemanfaatan > Teknologi Aeronautika |
| Divisions: | LAPAN > Deputi Teknologi Penerbangan Dan Antariksa > Pusat Teknologi Roket > Balai Uji Teknologi Dan Pengamatan Antariksa Dan Atmosfer Garut |
| Depositing User: | Administrator Repository |
| Date Deposited: | 15 Jun 2021 05:00 |
| Last Modified: | 18 Jul 2022 08:10 |
| URI: | https://karya.brin.go.id/id/eprint/11768 |
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