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...

Full description

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:
Online Access: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
_version_ 1848786529403535360
author Salleh, Hafiz
Saharin, Sanisah
Azmi, Mohammad Hanafi
Khan, Sher Afghan
author_facet Salleh, Hafiz
Saharin, Sanisah
Azmi, Mohammad Hanafi
Khan, Sher Afghan
author_sort Salleh, Hafiz
building IIUM Repository
collection Online Access
description 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 (pencentage) is validated with experimental result from previous study. Effect of the change of wingspan on low Reynold number/flows is investigated for the wing lift coefficient, and aerodynamics efficiency. Some contour results including pressure contour is observed. The pressure contour along wingspan from each case is figured out.
first_indexed 2025-11-14T17:10:29Z
format Article
id iium-66198
institution International Islamic University Malaysia
institution_category Local University
language English
English
last_indexed 2025-11-14T17:10:29Z
publishDate 2018
publisher Science Publishing CorporationPublisher of International Academic Journals
recordtype eprints
repository_type Digital Repository
spelling iium-661982018-10-02T06:27:03Z http://irep.iium.edu.my/66198/ Fluid-structure interactions of variable span wings in low Reynold flows Salleh, Hafiz Saharin, Sanisah Azmi, Mohammad Hanafi Khan, Sher Afghan TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics 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 (pencentage) is validated with experimental result from previous study. Effect of the change of wingspan on low Reynold number/flows is investigated for the wing lift coefficient, and aerodynamics efficiency. Some contour results including pressure contour is observed. The pressure contour along wingspan from each case is figured out. Science Publishing CorporationPublisher of International Academic Journals 2018-08 Article PeerReviewed application/pdf en http://irep.iium.edu.my/66198/1/66198_Fluid-structure%20interactions%20of%20variable.pdf application/pdf en http://irep.iium.edu.my/66198/2/66198_Fluid-structure%20interactions%20of%20variable_SCOPUS.pdf Salleh, Hafiz and Saharin, Sanisah and Azmi, Mohammad Hanafi and Khan, Sher Afghan (2018) Fluid-structure interactions of variable span wings in low Reynold flows. International Journal of Engineering & Technology, 7 (3.29). pp. 381-385. ISSN 2227-524X https://www.sciencepubco.com/index.php/ijet/article/view/19198/8842 10.14419/ijet.v7i3.29.19198
spellingShingle TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
Salleh, Hafiz
Saharin, Sanisah
Azmi, Mohammad Hanafi
Khan, Sher Afghan
Fluid-structure interactions of variable span wings in low Reynold flows
title Fluid-structure interactions of variable span wings in low Reynold flows
title_full Fluid-structure interactions of variable span wings in low Reynold flows
title_fullStr Fluid-structure interactions of variable span wings in low Reynold flows
title_full_unstemmed Fluid-structure interactions of variable span wings in low Reynold flows
title_short Fluid-structure interactions of variable span wings in low Reynold flows
title_sort fluid-structure interactions of variable span wings in low reynold flows
topic TL Motor vehicles. Aeronautics. Astronautics
TL500 Aeronautics
url 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