Modeling and structural analysis of three-dimensional wing

This paper attempts to discover the structural behavior of the wing imperiled to flowing loads through the voyage. The study uses a method in the form of finite element analysis of wing flexure distortion. As a first step, two wing models are established by captivating factual features, wing assembl...

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Main Authors:	Mohd Zakuan, Muhammad Amir Mirza, Aabid, Abdul, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	Blue Eyes Intelligence Engineering & Sciences Publication 2019
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/75894/ http://irep.iium.edu.my/75894/ http://irep.iium.edu.my/75894/ http://irep.iium.edu.my/75894/1/Amir-paper.pdf

id	iium-75894
recordtype	eprints
spelling	iium-758942019-12-04T08:46:31Z http://irep.iium.edu.my/75894/ Modeling and structural analysis of three-dimensional wing Mohd Zakuan, Muhammad Amir Mirza Aabid, Abdul Khan, Sher Afghan TL Motor vehicles. Aeronautics. Astronautics This paper attempts to discover the structural behavior of the wing imperiled to flowing loads through the voyage. The study uses a method in the form of finite element analysis of wing flexure distortion. As a first step, two wing models are established by captivating factual features, wing assembly, and plan principles into consideration. The gathering wing prototypical entails of the tinny membrane, two poles, and multi-ribs. Two spars which consist of primary and secondary spars. NACA 23015 is chosen as the baseline aerofoil as this is identical alike to the tailored aerofoil being castoff in Airbus A320. Two rods mostly endure the twisting moment and trim strength, which is finished of titanium contaminant to ensure enough inflexibility. The covering and wing spars are made of aluminum amalgam to lessen the structural heaviness. Later, a static structural investigation is smeared, and the overall distortion, comparable elastic strain, and corresponding Von-Mises tension are obtained to analyze the mechanical behavior of the wing. Furthermore, the modal investigation is being supported out to determine the natural rate of recurrence, as well as the modal shape of the three orders, which are acquired through the pre-stress modal analysis. The outcomes of the modal scrutiny aid engineers decrease excitation on the natural occurrences and avert the wing from the flurry. In view of the results obtained from the study, designers can emphasize consolidation and analysis of the stress attentiveness range and huge distortion area. In conclusion, the recreation consequences indicate that the arrangement is possible and improves the information grade of the lifting surface. Blue Eyes Intelligence Engineering & Sciences Publication 2019-11-04 Article PeerReviewed application/pdf en http://irep.iium.edu.my/75894/1/Amir-paper.pdf Mohd Zakuan, Muhammad Amir Mirza and Aabid, Abdul and Khan, Sher Afghan (2019) Modeling and structural analysis of three-dimensional wing. International Journal of Engineering and Advanced Technology (IJEAT), 9 (1). pp. 6820-6828. ISSN 2249-8958 https://www.ijeat.org/wp-content/uploads/papers/v9i1/A2983109119.pdf 10.35940/ijeat.A2983.109119
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Mohd Zakuan, Muhammad Amir Mirza Aabid, Abdul Khan, Sher Afghan Modeling and structural analysis of three-dimensional wing
description	This paper attempts to discover the structural behavior of the wing imperiled to flowing loads through the voyage. The study uses a method in the form of finite element analysis of wing flexure distortion. As a first step, two wing models are established by captivating factual features, wing assembly, and plan principles into consideration. The gathering wing prototypical entails of the tinny membrane, two poles, and multi-ribs. Two spars which consist of primary and secondary spars. NACA 23015 is chosen as the baseline aerofoil as this is identical alike to the tailored aerofoil being castoff in Airbus A320. Two rods mostly endure the twisting moment and trim strength, which is finished of titanium contaminant to ensure enough inflexibility. The covering and wing spars are made of aluminum amalgam to lessen the structural heaviness. Later, a static structural investigation is smeared, and the overall distortion, comparable elastic strain, and corresponding Von-Mises tension are obtained to analyze the mechanical behavior of the wing. Furthermore, the modal investigation is being supported out to determine the natural rate of recurrence, as well as the modal shape of the three orders, which are acquired through the pre-stress modal analysis. The outcomes of the modal scrutiny aid engineers decrease excitation on the natural occurrences and avert the wing from the flurry. In view of the results obtained from the study, designers can emphasize consolidation and analysis of the stress attentiveness range and huge distortion area. In conclusion, the recreation consequences indicate that the arrangement is possible and improves the information grade of the lifting surface.
format	Article
author	Mohd Zakuan, Muhammad Amir Mirza Aabid, Abdul Khan, Sher Afghan
author_facet	Mohd Zakuan, Muhammad Amir Mirza Aabid, Abdul Khan, Sher Afghan
author_sort	Mohd Zakuan, Muhammad Amir Mirza
title	Modeling and structural analysis of three-dimensional wing
title_short	Modeling and structural analysis of three-dimensional wing
title_full	Modeling and structural analysis of three-dimensional wing
title_fullStr	Modeling and structural analysis of three-dimensional wing
title_full_unstemmed	Modeling and structural analysis of three-dimensional wing
title_sort	modeling and structural analysis of three-dimensional wing
publisher	Blue Eyes Intelligence Engineering & Sciences Publication
publishDate	2019
url	http://irep.iium.edu.my/75894/ http://irep.iium.edu.my/75894/ http://irep.iium.edu.my/75894/ http://irep.iium.edu.my/75894/1/Amir-paper.pdf
first_indexed	2023-09-18T21:47:21Z
last_indexed	2023-09-18T21:47:21Z
_version_	1777413538283782144

Modeling and structural analysis of three-dimensional wing

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