Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device

Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device

A six component force balance was used to obtain the aerodynamic performance of a NACA 23012 half wing model with a slender reverse delta type add-on device in landing configuration (slat deflection 15° and flap deflection 20°) at a chord-based Reynolds number of Rec =2.74×105. Reverse delta type...

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Bibliographic Details
Main Authors: Asrar, Waqar, Altaf, Afaq, Omar, Ashraf Ali, Hrairi, Meftah, Thong , Boon Tan
Format: Conference or Workshop Item
Language:English
English
Published: 2015
Subjects:
TL500 Aeronautics
Online Access:http://irep.iium.edu.my/46153/
http://irep.iium.edu.my/46153/1/AIAC-2015-040.pdf
http://irep.iium.edu.my/46153/4/AIAC_2015_Ankara_conference.docx
id iium-46153
recordtype eprints
spelling iium-461532016-07-18T09:05:11Z http://irep.iium.edu.my/46153/ Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device Asrar, Waqar Altaf, Afaq Omar, Ashraf Ali Hrairi, Meftah Thong , Boon Tan TL500 Aeronautics A six component force balance was used to obtain the aerodynamic performance of a NACA 23012 half wing model with a slender reverse delta type add-on device in landing configuration (slat deflection 15° and flap deflection 20°) at a chord-based Reynolds number of Rec =2.74×105. Reverse delta type add-on devices of three different sizes were tested. It was found that the aerodynamic performance of the half wing model was only slightly affected by the use of a reverse delta type addon device. It was found that the reduction in lift is 4.9% and the increase in drag is 15.2%. 2015-09-10 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/46153/1/AIAC-2015-040.pdf application/pdf en http://irep.iium.edu.my/46153/4/AIAC_2015_Ankara_conference.docx Asrar, Waqar and Altaf, Afaq and Omar, Ashraf Ali and Hrairi, Meftah and Thong , Boon Tan (2015) Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device. In: 8th Ankara International Aerospace Conference, 10-12 Sep 2015, Ankara, Turkey.
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
English
topic TL500 Aeronautics
spellingShingle TL500 Aeronautics
Asrar, Waqar
Altaf, Afaq
Omar, Ashraf Ali
Hrairi, Meftah
Thong , Boon Tan
Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
description A six component force balance was used to obtain the aerodynamic performance of a NACA 23012 half wing model with a slender reverse delta type add-on device in landing configuration (slat deflection 15° and flap deflection 20°) at a chord-based Reynolds number of Rec =2.74×105. Reverse delta type add-on devices of three different sizes were tested. It was found that the aerodynamic performance of the half wing model was only slightly affected by the use of a reverse delta type addon device. It was found that the reduction in lift is 4.9% and the increase in drag is 15.2%.
format Conference or Workshop Item
author Asrar, Waqar
Altaf, Afaq
Omar, Ashraf Ali
Hrairi, Meftah
Thong , Boon Tan
author_facet Asrar, Waqar
Altaf, Afaq
Omar, Ashraf Ali
Hrairi, Meftah
Thong , Boon Tan
author_sort Asrar, Waqar
title Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
title_short Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
title_full Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
title_fullStr Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
title_full_unstemmed Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
title_sort aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
publishDate 2015
url http://irep.iium.edu.my/46153/
http://irep.iium.edu.my/46153/1/AIAC-2015-040.pdf
http://irep.iium.edu.my/46153/4/AIAC_2015_Ankara_conference.docx
first_indexed 2023-09-18T21:05:43Z
last_indexed 2023-09-18T21:05:43Z
_version_ 1777410919188398080

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