Numerical investigation of the effect of spoiler’s configuration on wake vortex
A numerical investigation was undertaken to study the aerodynamic characteristics of wake vortices generated from an aircraft during taking-off or landing, and thus exploring the possible techniques of reducing hazard imposed to the following aircraft by means of passive wake vortex alleviation by u...
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| Format: | Monograph |
| Language: | English |
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2012
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| Online Access: | http://irep.iium.edu.my/35597/ http://irep.iium.edu.my/35597/ http://irep.iium.edu.my/35597/1/EDW_B11-027-0505.pdf |
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iium-35597 |
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eprints |
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iium-355972016-10-20T03:05:57Z http://irep.iium.edu.my/35597/ Numerical investigation of the effect of spoiler’s configuration on wake vortex Omar, Ashraf Ali E. Asrar, Waqar Ludin @Jamaluddin, Hani T Technology (General) A numerical investigation was undertaken to study the aerodynamic characteristics of wake vortices generated from an aircraft during taking-off or landing, and thus exploring the possible techniques of reducing hazard imposed to the following aircraft by means of passive wake vortex alleviation by using delta wing (DW) as an add-on device. Simulations were performed using RANS turbulence model. 2012-05 Monograph NonPeerReviewed application/pdf en http://irep.iium.edu.my/35597/1/EDW_B11-027-0505.pdf Omar, Ashraf Ali E. and Asrar, Waqar and Ludin @Jamaluddin, Hani (2012) Numerical investigation of the effect of spoiler’s configuration on wake vortex. Research Report. UNSPECIFIED. (Unpublished) EDW B11-027-0505 |
| repository_type |
Digital Repository |
| institution_category |
Local University |
| institution |
International Islamic University Malaysia |
| building |
IIUM Repository |
| collection |
Online Access |
| language |
English |
| topic |
T Technology (General) |
| spellingShingle |
T Technology (General) Omar, Ashraf Ali E. Asrar, Waqar Ludin @Jamaluddin, Hani Numerical investigation of the effect of spoiler’s configuration on wake vortex |
| description |
A numerical investigation was undertaken to study the aerodynamic characteristics of wake vortices generated from an aircraft during taking-off or landing, and thus exploring the possible techniques of reducing hazard imposed to the following aircraft by means of passive wake vortex alleviation by using delta wing (DW) as an add-on device. Simulations were performed using RANS turbulence model. |
| format |
Monograph |
| author |
Omar, Ashraf Ali E. Asrar, Waqar Ludin @Jamaluddin, Hani |
| author_facet |
Omar, Ashraf Ali E. Asrar, Waqar Ludin @Jamaluddin, Hani |
| author_sort |
Omar, Ashraf Ali E. |
| title |
Numerical investigation of the effect of spoiler’s configuration on wake vortex |
| title_short |
Numerical investigation of the effect of spoiler’s configuration on wake vortex |
| title_full |
Numerical investigation of the effect of spoiler’s configuration on wake vortex |
| title_fullStr |
Numerical investigation of the effect of spoiler’s configuration on wake vortex |
| title_full_unstemmed |
Numerical investigation of the effect of spoiler’s configuration on wake vortex |
| title_sort |
numerical investigation of the effect of spoiler’s configuration on wake vortex |
| publishDate |
2012 |
| url |
http://irep.iium.edu.my/35597/ http://irep.iium.edu.my/35597/ http://irep.iium.edu.my/35597/1/EDW_B11-027-0505.pdf |
| first_indexed |
2023-09-18T20:51:00Z |
| last_indexed |
2023-09-18T20:51:00Z |
| _version_ |
1777409993849438208 |