Aerodynamics of porous airfoils and wings

This paper presents novel wind tunnel test results on the aerodynamics of a symmetric thin porous airfoil and a porous rectangular half wing using a symmetric thin airfoil as its cross section, obtained by a six-component force balance. The variation of lift coefficient, drag coefficient, pitching...

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Main Authors:	Mohammed Aldheeb, Mohammed Abdulmalek, Asrar, Waqar, Sulaeman, Erwin, Omar, Ashraf Ali
Format:	Article
Language:	English English English
Published:	SpringerLink 2018
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/1/Aerodynamics%20of%20permeable%20airfoils%20and%20wings-published.pdf http://irep.iium.edu.my/64676/7/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_SCOPUS.pdf http://irep.iium.edu.my/64676/13/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_WOS.pdf

id	iium-64676
recordtype	eprints
spelling	iium-646762019-12-09T06:57:49Z http://irep.iium.edu.my/64676/ Aerodynamics of porous airfoils and wings Mohammed Aldheeb, Mohammed Abdulmalek Asrar, Waqar Sulaeman, Erwin Omar, Ashraf Ali TL500 Aeronautics This paper presents novel wind tunnel test results on the aerodynamics of a symmetric thin porous airfoil and a porous rectangular half wing using a symmetric thin airfoil as its cross section, obtained by a six-component force balance. The variation of lift coefficient, drag coefficient, pitching moment, lift versus drag, the gradient of lift, and location of the aerodynamic center with respect to the angle of attack are presented as a function of the porosity. The data, where possible, are compared with the analytical results. The trend of the experimental results behaves in the same manner as the analytical solution. The measured drag coefficients of the airfoil and wing are also presented. The applicability of the standard equation relating the lift coefficient of a non-porous wing with that of a non-porous airfoil to the case of porous wings is verified by applying the equation to porous wings and validating the results using experimental data. Lift slope decreases as the porosity increases. The drag decreases at a low value of porosity and then increases as porosity increases. The standard equation for obtaining the lift coefficient of a wing from the lift coefficient of an airfoil is applicable and valid for porous wings and airfoils. SpringerLink 2018-07-04 Article PeerReviewed application/pdf en http://irep.iium.edu.my/64676/1/Aerodynamics%20of%20permeable%20airfoils%20and%20wings-published.pdf application/pdf en http://irep.iium.edu.my/64676/7/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_SCOPUS.pdf application/pdf en http://irep.iium.edu.my/64676/13/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_WOS.pdf Mohammed Aldheeb, Mohammed Abdulmalek and Asrar, Waqar and Sulaeman, Erwin and Omar, Ashraf Ali (2018) Aerodynamics of porous airfoils and wings. Acta Mechanica, online 1st. pp. 1-19. ISSN 0001-5970 E-ISSN 1619-6937 (In Press) https://link.springer.com/article/10.1007/s00707-018-2203-6 10.1007/s00707-018-2203-6
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics Mohammed Aldheeb, Mohammed Abdulmalek Asrar, Waqar Sulaeman, Erwin Omar, Ashraf Ali Aerodynamics of porous airfoils and wings
description	This paper presents novel wind tunnel test results on the aerodynamics of a symmetric thin porous airfoil and a porous rectangular half wing using a symmetric thin airfoil as its cross section, obtained by a six-component force balance. The variation of lift coefficient, drag coefficient, pitching moment, lift versus drag, the gradient of lift, and location of the aerodynamic center with respect to the angle of attack are presented as a function of the porosity. The data, where possible, are compared with the analytical results. The trend of the experimental results behaves in the same manner as the analytical solution. The measured drag coefficients of the airfoil and wing are also presented. The applicability of the standard equation relating the lift coefficient of a non-porous wing with that of a non-porous airfoil to the case of porous wings is verified by applying the equation to porous wings and validating the results using experimental data. Lift slope decreases as the porosity increases. The drag decreases at a low value of porosity and then increases as porosity increases. The standard equation for obtaining the lift coefficient of a wing from the lift coefficient of an airfoil is applicable and valid for porous wings and airfoils.
format	Article
author	Mohammed Aldheeb, Mohammed Abdulmalek Asrar, Waqar Sulaeman, Erwin Omar, Ashraf Ali
author_facet	Mohammed Aldheeb, Mohammed Abdulmalek Asrar, Waqar Sulaeman, Erwin Omar, Ashraf Ali
author_sort	Mohammed Aldheeb, Mohammed Abdulmalek
title	Aerodynamics of porous airfoils and wings
title_short	Aerodynamics of porous airfoils and wings
title_full	Aerodynamics of porous airfoils and wings
title_fullStr	Aerodynamics of porous airfoils and wings
title_full_unstemmed	Aerodynamics of porous airfoils and wings
title_sort	aerodynamics of porous airfoils and wings
publisher	SpringerLink
publishDate	2018
url	http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/ http://irep.iium.edu.my/64676/1/Aerodynamics%20of%20permeable%20airfoils%20and%20wings-published.pdf http://irep.iium.edu.my/64676/7/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_SCOPUS.pdf http://irep.iium.edu.my/64676/13/64676_Aerodynamics%20of%20porous%20airfoils%20and%20wings_WOS.pdf
first_indexed	2023-09-18T21:31:47Z
last_indexed	2023-09-18T21:31:47Z
_version_	1777412558933721088

Aerodynamics of porous airfoils and wings

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