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...
| Main Authors: | , , , , |
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| Format: | Proceeding Paper |
| Language: | English English |
| Published: |
2015
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| Subjects: | |
| 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 |
| _version_ | 1848782917998739456 |
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| 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 |
| building | IIUM Repository |
| collection | Online Access |
| 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%. |
| first_indexed | 2025-11-14T16:13:05Z |
| format | Proceeding Paper |
| id | iium-46153 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English English |
| last_indexed | 2025-11-14T16:13:05Z |
| publishDate | 2015 |
| recordtype | eprints |
| repository_type | Digital Repository |
| 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 Proceeding Paper 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. |
| 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 |
| title | 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_short | 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 |
| topic | TL500 Aeronautics |
| 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 |