The unmanned aerial vehicle (UAV) has been widely utilized all over the world for either civil or military purposes. For civil purpose, UAV can be used for maritime surveillance to prevent illegal fishing happens in Indonesia. The purpose of this paper is to analyze the composite wing structure of the maritime surveillance UAV using finite element model. The load is assumed as static and distributed along semi span using Schrenk method. In finite element model, the wing is modeled using quad4 element and boundary condition used pin in the locations where bolts will be applied. Verification, validation and mesh convergence test take into account to obtain good results from finite element model application. The analysis is conducted with load factor of 3.8 and -1.52 which represent maximum and minimum load factor. Based on the results, the wing composite structure of the maritime surveillance UAV is safe because it has factor of safety of 1.66 for load factor 3.8 and 3.35 for load factor -1.52 based on Tsai-Wu failure criterion. Meanwhile displacement in y direction for load factor 3.8 and -1.52 are 97.1 mm and -38.8 mm respectively.
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6 May 2020
RECENT PROGRESS ON: MECHANICAL, INFRASTRUCTURE AND INDUSTRIAL ENGINEERING: Proceedings of International Symposium on Advances in Mechanical Engineering (ISAME): Quality in Research 2019
22–24 July 2019
Padang, Indonesia
Research Article|
May 06 2020
Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle
Fajar Ari Wandono;
Fajar Ari Wandono
b)
1
Research Center for Advanced Vehicle (RCAVe) Universitas Indonesia
, Indonesia
16424
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Mohammad Adhitya
Mohammad Adhitya
a)
1
Research Center for Advanced Vehicle (RCAVe) Universitas Indonesia
, Indonesia
16424a)Corresponding author: [email protected]
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a)Corresponding author: [email protected]
AIP Conf. Proc. 2227, 020029 (2020)
Citation
Fajar Ari Wandono, Mohammad Adhitya; Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle. AIP Conf. Proc. 6 May 2020; 2227 (1): 020029. https://doi.org/10.1063/5.0003760
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