Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle

Autor: Basri, Ernnie Illyani, Mustapha, Faizal, Sultan, Mohamed Thariq Hameed, Basri, Adi Azriff, Abas, Mohd Firdaus, Majid, Mohd Shukry Abdul, Ahmad, Kamarul Arifin
Zdroj: In Journal of Materials Research and Technology September-October 2019 8(5):4374-4386
Databáze: ScienceDirect