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Modal analysis of UAV aircraft structures with different tail configurations

Modal analysis of UAV aircraft structures with different tail configurations / Nurul Aqmal Syuhaida Azlan
Kertas kerja ini dihasilkan untuk menganalisis struktur kenderaan pesawat udara tanpa pemandu menggunakan analisis modal dengan menggunakan perisian ANSYS Mechanical APDL yang memerlukan pelajar yang pengalaman dan mempunyai pemahaman asas perisian ANSYS Mechanical APDL. Masalah unsur rasuk tiga dimensi dianggap memudahkan pembangunan yang memberi penekanan kepada prosedur yang teratur yang melibatkan konsep elemen penting seperti kekerapan semula jadi, dan bentuk mod dengan menggunakan hasil ANSYS Mechanical APDL. Keupayaan ANSYS untuk memanipulasi reka bentuk kenderaan udara tanpa pemandu dengan konfigurasi yang berlainan yang membuat analisis lebih ringkas dan mudah untuk digunakan. Fleksibiliti dalam analisis unsur terhingga dengan ANSYS Mechanical APDL melalui pelaksanaan komputer membolehkan sebahagian besar masalah yang perlu diubahsuai dengan mudah ke dalam projek-projek reka bentuk. _______________________________________________________________________________________________________ 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.
Contributor(s):
Nurul Aqmal Syuhaida Azlan - Author
Primary Item Type:
Final Year Project
Identifiers:
Accession Number : 875007325
Barcode : 00003107204
Language:
English
Subject Keywords:
aircraft structures; unmanned aerial vehicle; ANSYS Mechanical APDL
First presented to the public:
6/1/2017
Original Publication Date:
3/16/2018
Previously Published By:
Universiti Sains Malaysia
Place Of Publication:
School of Aerospace Engineering
Citation:
Extents:
Number of Pages - 73
License Grantor / Date Granted:
  / ( View License )
Date Deposited
2018-03-16 16:50:55.562
Date Last Updated
2020-05-06 16:27:18.943
Submitter:
Mohd Jasnizam Mohd Salleh

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