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

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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Bibliographic Details
Main Authors: Basri, Ernnie Illyani, Basri, Adi Azriff, Abas, Mohd. Firdaus, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Ahmad, Kamarul Arifin
Format: Article
Language:English
Published: Penerbit Akademia Baru 2019
Online Access: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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Institution: Universiti Putra Malaysia
Language: English

Internet

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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