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

A finite element model is developed to determine deformation and stresses on a composite wing of unmanned aerial vehicle (UAV) with a tubercle design at the leading edge of the wing. Tubercles, commonly known as protuberances found on the leading edge of a whale pectoral flipper, offering great perf...

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書誌詳細
主要な著者:	Basri, Ernnie Illyani, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Basri, Adi Azriff, Abas, Mohd Firdaus, Abdul Majid, Mohd Shukry, Ahmad, Kamarul Arifin
フォーマット:	論文
言語:	English
出版事項:	Elsevier 2019
オンライン･アクセス:	http://psasir.upm.edu.my/id/eprint/81007/1/FINITE.pdf http://psasir.upm.edu.my/id/eprint/81007/ https://www.sciencedirect.com/science/article/pii/S2238785419301413
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