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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2015
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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. |
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International Islamic University Malaysia |
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language |
English English |
topic |
TL500 Aeronautics |
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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 |