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

• 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

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...