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

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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Bibliographic Details
Main Authors: Salleh, Hafiz, Saharin, Sanisah, Azmi, Mohammad Hanafi, Khan, Sher Afghan
Format: Article
Language:English
English
Published: Science Publishing CorporationPublisher of International Academic Journals 2018
Subjects:
TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
Online Access:http://irep.iium.edu.my/66198/
http://irep.iium.edu.my/66198/
http://irep.iium.edu.my/66198/
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
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http://irep.iium.edu.my/66198/
http://irep.iium.edu.my/66198/
http://irep.iium.edu.my/66198/
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

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