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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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Main Authors:	Basri, Ernnie Illyani, Basri, Adi Azriff, Abas, Mohd. Firdaus, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Ahmad, Kamarul Arifin
格式:	Article
语言:	English
出版:	Penerbit Akademia Baru 2019
在线阅读:	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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