Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.

In this project, finite element analysis (FEA) of the swept wing structure of an Unmanned Aerial Vehicle (UAV) for target drone purpose was performed. This project is very significant as it helps us to predict the behavior of a wing structure under a certain condition using FEA software MSC PATRAN a...

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Main Author:	Abd Wahab, Fairul Adzreen
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Finite element method Machine design and drawing
Online Access:	https://ir.uitm.edu.my/id/eprint/31151/1/31151.pdf
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id	my-uitm-ir.31151
record_format	uketd_dc
spelling	my-uitm-ir.311512024-04-19T02:41:03Z Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab. 2009 Abd Wahab, Fairul Adzreen Finite element method Machine design and drawing In this project, finite element analysis (FEA) of the swept wing structure of an Unmanned Aerial Vehicle (UAV) for target drone purpose was performed. This project is very significant as it helps us to predict the behavior of a wing structure under a certain condition using FEA software MSC PATRAN and NASTRAN. For the purpose of finite element modeling, the CATIA file of the wing structure was imported into MSC PATRAN. The structure was then meshed using combination of CQUAD4 and TRIA3 elements. Aluminum alloys such 2024-T3 and AISI 4140 Steel with various thicknesses are employed for the wing structure sustaining Maximum Take-Off Weight of 250 kg under 4G loading condition. It was found that the maximum von Misses stress occurs on the vicinity of the connection between the wing and the fuselage, meanwhile the maximum displacement occurs at the tip of the wing structure. The results of the analysis were then checked·using manual analysis to find the stress on a specific point on the wing structure and compared to the I computational result. The structure will fail if stress is greater than the yield strength of the material used. These have proved that by using finite elements analysis, the behavior of structures can be predicted before they are to be produced. 2009 Thesis https://ir.uitm.edu.my/id/eprint/31151/ https://ir.uitm.edu.my/id/eprint/31151/1/31151.pdf text en public degree Universiti Teknologi MARA Shah Alam Faculty of Mechanical Engineering Kuntjoro, Wahyu (Prof. Dr. Ir.)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Kuntjoro, Wahyu (Prof. Dr. Ir.)
topic	Finite element method Machine design and drawing
spellingShingle	Finite element method Machine design and drawing Abd Wahab, Fairul Adzreen Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.
description	In this project, finite element analysis (FEA) of the swept wing structure of an Unmanned Aerial Vehicle (UAV) for target drone purpose was performed. This project is very significant as it helps us to predict the behavior of a wing structure under a certain condition using FEA software MSC PATRAN and NASTRAN. For the purpose of finite element modeling, the CATIA file of the wing structure was imported into MSC PATRAN. The structure was then meshed using combination of CQUAD4 and TRIA3 elements. Aluminum alloys such 2024-T3 and AISI 4140 Steel with various thicknesses are employed for the wing structure sustaining Maximum Take-Off Weight of 250 kg under 4G loading condition. It was found that the maximum von Misses stress occurs on the vicinity of the connection between the wing and the fuselage, meanwhile the maximum displacement occurs at the tip of the wing structure. The results of the analysis were then checked·using manual analysis to find the stress on a specific point on the wing structure and compared to the I computational result. The structure will fail if stress is greater than the yield strength of the material used. These have proved that by using finite elements analysis, the behavior of structures can be predicted before they are to be produced.
format	Thesis
qualification_level	Bachelor degree
author	Abd Wahab, Fairul Adzreen
author_facet	Abd Wahab, Fairul Adzreen
author_sort	Abd Wahab, Fairul Adzreen
title	Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.
title_short	Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.
title_full	Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.
title_fullStr	Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.
title_full_unstemmed	Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.
title_sort	finite element analysis of high subsonic air target drone wing structure (high swept configuration) / fairul adzreen abd wahab.
granting_institution	Universiti Teknologi MARA Shah Alam
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/31151/1/31151.pdf
_version_	1804889623710662656

Finite element analysis of high subsonic air target drone wing structure (high swept configuration) / Fairul Adzreen Abd Wahab.

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