Modal Analysis Of UAV Aircraft Structures With Different Tail Configurations

Azlan, Nurul Aqmal Syuhaida (2017) Modal Analysis Of UAV Aircraft Structures With Different Tail Configurations. Project Report. Universiti Sains Malaysia, Pusat Pengajian Kejuruteraan Aeroangkasa. (Submitted)

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Abstract

This thesis is to analyze the unmanned aerial vehicle aircraft structures using the modal analysis by using ANSYS Mechanical APDL software which requires an experienced student and the fundamental understanding of the ANSYS Mechanical APDL software. The three-dimensional beam element problems are considered to simplify the development which emphasizes on orderly procedure that involves the important element concepts such as natural frequency, and mode shape by using ANSYS Mechanical APDL result. The ANSYS’s ability to manipulate the design of the unmanned aerial vehicle with different configurations which makes the analysis more concise and easy to use. The flexibility of the Finite Element Analysis with ANSYS Mechanical APDL through the computer implementation allows most of the problems to be easily modified into design projects.

Item Type:	Monograph (Project Report)
Subjects:	T Technology
Divisions:	Kampus Kejuruteraan (Engineering Campus) > Pusat Pengajian Kejuruteraan Aeroangkasa (School of Aerospace Engineering) > Monograph
Depositing User:	Mr Mohamed Yunus Mat Yusof
Date Deposited:	28 Feb 2022 02:12
Last Modified:	28 Feb 2022 02:12
URI:	http://eprints.usm.my/id/eprint/51689

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