Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle

Fajar Ari Wandono; Mohammad Adhitya

doi:10.1063/5.0003760

Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle

Fajar Ari Wandono, Mohammad Adhitya

Department of Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

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.

Original language	English
Title of host publication	Recent Progress on
Subtitle of host publication	Mechanical, Infrastructure and Industrial Engineering - Proceedings of the International Symposium on Advances in Mechanical Engineering, ISAME 2019: Quality in Research 2019
Editors	Nahry, Dwinanti Rika Marthanty
Publisher	American Institute of Physics Inc.
ISBN (Electronic)	9780735419865
DOIs	https://doi.org/10.1063/5.0003760
Publication status	Published - 6 May 2020
Event	16th International Conference on Quality in Research, QiR 2019 - 2019 International Symposium on Advances in Mechanical Engineering, ISAME 2019 - Padang, Indonesia Duration: 22 Jul 2019 → 24 Jul 2019

Publication series

Name	AIP Conference Proceedings
Volume	2227
ISSN (Print)	0094-243X
ISSN (Electronic)	1551-7616

Conference

Conference	16th International Conference on Quality in Research, QiR 2019 - 2019 International Symposium on Advances in Mechanical Engineering, ISAME 2019
Country/Territory	Indonesia
City	Padang
Period	22/07/19 → 24/07/19

Access to Document

10.1063/5.0003760

Cite this

Wandono, F. A., & Adhitya, M. (2020). Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle. In Nahry, & D. R. Marthanty (Eds.), Recent Progress on: Mechanical, Infrastructure and Industrial Engineering - Proceedings of the International Symposium on Advances in Mechanical Engineering, ISAME 2019: Quality in Research 2019 Article 020029 (AIP Conference Proceedings; Vol. 2227). American Institute of Physics Inc.. https://doi.org/10.1063/5.0003760

Wandono, Fajar Ari ; Adhitya, Mohammad. / Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle. Recent Progress on: Mechanical, Infrastructure and Industrial Engineering - Proceedings of the International Symposium on Advances in Mechanical Engineering, ISAME 2019: Quality in Research 2019. editor / Nahry ; Dwinanti Rika Marthanty. American Institute of Physics Inc., 2020. (AIP Conference Proceedings).

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title = "Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle",

abstract = "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. ",

author = "Wandono, {Fajar Ari} and Mohammad Adhitya",

note = "Funding Information: The authors would like to thank PITTA 2019 grant program of the Universitas Indonesia for funding this research and also Aeronautics Technology Center (Pustekbang) LAPAN for the UAV data. Publisher Copyright: {\textcopyright} 2020 Author(s). Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 16th International Conference on Quality in Research, QiR 2019 - 2019 International Symposium on Advances in Mechanical Engineering, ISAME 2019 ; Conference date: 22-07-2019 Through 24-07-2019",

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Wandono, FA & Adhitya, M 2020, Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle. in Nahry & DR Marthanty (eds), Recent Progress on: Mechanical, Infrastructure and Industrial Engineering - Proceedings of the International Symposium on Advances in Mechanical Engineering, ISAME 2019: Quality in Research 2019., 020029, AIP Conference Proceedings, vol. 2227, American Institute of Physics Inc., 16th International Conference on Quality in Research, QiR 2019 - 2019 International Symposium on Advances in Mechanical Engineering, ISAME 2019, Padang, Indonesia, 22/07/19. https://doi.org/10.1063/5.0003760

Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle. / Wandono, Fajar Ari; Adhitya, Mohammad.
Recent Progress on: Mechanical, Infrastructure and Industrial Engineering - Proceedings of the International Symposium on Advances in Mechanical Engineering, ISAME 2019: Quality in Research 2019. ed. / Nahry; Dwinanti Rika Marthanty. American Institute of Physics Inc., 2020. 020029 (AIP Conference Proceedings; Vol. 2227).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Wandono, Fajar Ari

AU - Adhitya, Mohammad

N1 - Funding Information: The authors would like to thank PITTA 2019 grant program of the Universitas Indonesia for funding this research and also Aeronautics Technology Center (Pustekbang) LAPAN for the UAV data. Publisher Copyright: © 2020 Author(s). Copyright: Copyright 2020 Elsevier B.V., All rights reserved.

PY - 2020/5/6

Y1 - 2020/5/6

N2 - 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.

AB - 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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A2 - Nahry, null

A2 - Marthanty, Dwinanti Rika

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T2 - 16th International Conference on Quality in Research, QiR 2019 - 2019 International Symposium on Advances in Mechanical Engineering, ISAME 2019

Y2 - 22 July 2019 through 24 July 2019

ER -

Wandono FA, Adhitya M. Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle. In Nahry, Marthanty DR, editors, Recent Progress on: Mechanical, Infrastructure and Industrial Engineering - Proceedings of the International Symposium on Advances in Mechanical Engineering, ISAME 2019: Quality in Research 2019. American Institute of Physics Inc. 2020. 020029. (AIP Conference Proceedings). doi: 10.1063/5.0003760

Finite element analysis for composite wing structure of the maritime surveillance unmanned aerial vehicle

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