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UAV NACA4415 wing structural performance analysis subjected to external aerodynamic load using Schrenk’s approximation

Structural analysis is widely used in the analysis of aircraft structures with the common application of the finite element method. The optimum structural design of aircraft wing is the crucial aspect in the performance of the aircraft considering the high stiffness-to-weight...

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書誌詳細
主要な著者:	Basri, Ernnie Illyani, Basri, Adi Azriff, Abas, Mohd. Firdaus, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Ahmad, Kamarul Arifin
フォーマット:	論文
言語:	English
出版事項:	Penerbit Akademia Baru 2019
オンライン･アクセス:	http://psasir.upm.edu.my/id/eprint/82455/1/UAV%20NACA4415%20wing%20.pdf http://psasir.upm.edu.my/id/eprint/82455/ https://akademiabaru.com/submit/index.php/arfmts/article/view/2642
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