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Fluid-structure interactions of variable span wings in low Reynold flows

Numerical method is one of the method which is applied to study the aerodynamics of static variable span morphing wing and to evaluate flow structure over the wing surface (especially leading edge) at different low reynolds number/flow. The numerical result of lift coefficient vs span increment (pen...

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書誌詳細
主要な著者:	Salleh, Hafiz, Saharin, Sanisah, Azmi, Mohammad Hanafi, Khan, Sher Afghan
フォーマット:	論文
言語:	English English
出版事項:	Science Publishing CorporationPublisher of International Academic Journals 2018
主題:	TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics
オンライン･アクセス:	http://irep.iium.edu.my/66198/1/66198_Fluid-structure%20interactions%20of%20variable.pdf http://irep.iium.edu.my/66198/2/66198_Fluid-structure%20interactions%20of%20variable_SCOPUS.pdf http://irep.iium.edu.my/66198/ https://www.sciencepubco.com/index.php/ijet/article/view/19198/8842
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