Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing

A low Reynolds number, three-dimensional CFD analysis is carried out for a finite flat plate wing using the commercial CFD code STAR CCM+. The six-aerodynamic force and moment components CL, CD, CM, CN, Cl, CY and their derivatives are computed at a Reynolds numbers of 3x105 by varying the pitch, ro...

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Main Authors:	Malik, Khurshid, Asrar, Waqar, Sulaeman, Erwin
Format:	Article
Language:	English English English
Published:	Embry Riddle Aeronautical University 2018
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/62270/ http://irep.iium.edu.my/62270/ http://irep.iium.edu.my/62270/7/62270_Low%20reynolds%20number%20numerical%20simulation_article.pdf http://irep.iium.edu.my/62270/8/62270_Low%20reynolds%20number%20numerical%20simulation_scopus.pdf http://irep.iium.edu.my/62270/19/62270_Low%20reynolds%20number%20numerical%20simulation_WoS.pdf

id	iium-62270
recordtype	eprints
spelling	iium-622702018-10-29T02:41:05Z http://irep.iium.edu.my/62270/ Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing Malik, Khurshid Asrar, Waqar Sulaeman, Erwin TL500 Aeronautics A low Reynolds number, three-dimensional CFD analysis is carried out for a finite flat plate wing using the commercial CFD code STAR CCM+. The six-aerodynamic force and moment components CL, CD, CM, CN, Cl, CY and their derivatives are computed at a Reynolds numbers of 3x105 by varying the pitch, roll and yaw angles about the quarter chord point. The computed results have been validated with experimental aerodynamic balance data when possible. The results indicate that roll and yaw angle affect the aerodynamic coefficients of the flat plate wing along with the pitch angle. The influence of roll and yaw angles on the six aerodynamics coefficients were found to be significant for high pitch angles specially 10 and 15. Stability derivatives have also been reported. This data is important for the design of MAVs and small UAVs and is currently perhaps not available in the open literature. Embry Riddle Aeronautical University 2018-02 Article PeerReviewed application/pdf en http://irep.iium.edu.my/62270/7/62270_Low%20reynolds%20number%20numerical%20simulation_article.pdf application/pdf en http://irep.iium.edu.my/62270/8/62270_Low%20reynolds%20number%20numerical%20simulation_scopus.pdf application/pdf en http://irep.iium.edu.my/62270/19/62270_Low%20reynolds%20number%20numerical%20simulation_WoS.pdf Malik, Khurshid and Asrar, Waqar and Sulaeman, Erwin (2018) Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing. International Journal of Aviation, Aeronautics, and Aerospace, 5 (1). pp. 1-27. ISSN 2374-6793 https://commons.erau.edu/cgi/viewcontent.cgi?article=1209&context=ijaaa
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 Malik, Khurshid Asrar, Waqar Sulaeman, Erwin Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
description	A low Reynolds number, three-dimensional CFD analysis is carried out for a finite flat plate wing using the commercial CFD code STAR CCM+. The six-aerodynamic force and moment components CL, CD, CM, CN, Cl, CY and their derivatives are computed at a Reynolds numbers of 3x105 by varying the pitch, roll and yaw angles about the quarter chord point. The computed results have been validated with experimental aerodynamic balance data when possible. The results indicate that roll and yaw angle affect the aerodynamic coefficients of the flat plate wing along with the pitch angle. The influence of roll and yaw angles on the six aerodynamics coefficients were found to be significant for high pitch angles specially 10 and 15. Stability derivatives have also been reported. This data is important for the design of MAVs and small UAVs and is currently perhaps not available in the open literature.
format	Article
author	Malik, Khurshid Asrar, Waqar Sulaeman, Erwin
author_facet	Malik, Khurshid Asrar, Waqar Sulaeman, Erwin
author_sort	Malik, Khurshid
title	Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
title_short	Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
title_full	Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
title_fullStr	Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
title_full_unstemmed	Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
title_sort	low reynolds number numerical simulation of the aerodynamic coefficients of a 3d wing
publisher	Embry Riddle Aeronautical University
publishDate	2018
url	http://irep.iium.edu.my/62270/ http://irep.iium.edu.my/62270/ http://irep.iium.edu.my/62270/7/62270_Low%20reynolds%20number%20numerical%20simulation_article.pdf http://irep.iium.edu.my/62270/8/62270_Low%20reynolds%20number%20numerical%20simulation_scopus.pdf http://irep.iium.edu.my/62270/19/62270_Low%20reynolds%20number%20numerical%20simulation_WoS.pdf
first_indexed	2023-09-18T21:28:17Z
last_indexed	2023-09-18T21:28:17Z
_version_	1777412338903678976

Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing

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