Numerical simulation of a low aspect ratio wing at low Reynolds number
In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. Commercial software STAR-CCM+ was used to simulate the flow and predict the aerodynamics performances of the low aspect ratio wing. Re...
| Main Authors: | , , , |
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| Format: | Proceeding Paper |
| Language: | English English |
| Published: |
2013
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/33139/ http://irep.iium.edu.my/33139/1/Paper_30161_-_Camera_ready.pdf http://irep.iium.edu.my/33139/4/programbookicmaae13.pdf |
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| author | Suliman , M. M. Ali Omar, Ashraf Ali Syed Mohamed Ali, Jaffar M. Syuhairi |, M. Husain |
| author_facet | Suliman , M. M. Ali Omar, Ashraf Ali Syed Mohamed Ali, Jaffar M. Syuhairi |, M. Husain |
| author_sort | Suliman , M. M. Ali |
| building | IIUM Repository |
| collection | Online Access |
| description | In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. Commercial software STAR-CCM+ was used to simulate the flow and predict the aerodynamics performances of the low aspect ratio wing. Results were presented in terms of pressure coefficient distribution, flow visualization, lift and drag coefficients for angle of attacks ranging from 0˚ to 18˚ and Reynolds numbers ranging from 104 to 105
Keywords: Rectangular planform wing; Tip vortices; Flow separation . The results showed that, for rectangular planform wing, the distribution of the pressure is dominated by vortices. The results also showed the formation of tip vortices at lower Reynolds number for rectangular wing configuration. It is evident from the results that the type of wing configurations plays a very important role in delaying or preventing the flow separation. |
| first_indexed | 2025-11-14T15:37:44Z |
| format | Proceeding Paper |
| id | iium-33139 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English English |
| last_indexed | 2025-11-14T15:37:44Z |
| publishDate | 2013 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | iium-331392013-12-09T03:46:50Z http://irep.iium.edu.my/33139/ Numerical simulation of a low aspect ratio wing at low Reynolds number Suliman , M. M. Ali Omar, Ashraf Ali Syed Mohamed Ali, Jaffar M. Syuhairi |, M. Husain TL500 Aeronautics In this work the numerical simulation of aerodynamic performance of low aspect ratio wings at low Reynolds numbers applicable to micro aerial vehicle is carried out. Commercial software STAR-CCM+ was used to simulate the flow and predict the aerodynamics performances of the low aspect ratio wing. Results were presented in terms of pressure coefficient distribution, flow visualization, lift and drag coefficients for angle of attacks ranging from 0˚ to 18˚ and Reynolds numbers ranging from 104 to 105 Keywords: Rectangular planform wing; Tip vortices; Flow separation . The results showed that, for rectangular planform wing, the distribution of the pressure is dominated by vortices. The results also showed the formation of tip vortices at lower Reynolds number for rectangular wing configuration. It is evident from the results that the type of wing configurations plays a very important role in delaying or preventing the flow separation. 2013 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/33139/1/Paper_30161_-_Camera_ready.pdf application/pdf en http://irep.iium.edu.my/33139/4/programbookicmaae13.pdf Suliman , M. M. Ali and Omar, Ashraf Ali and Syed Mohamed Ali, Jaffar and M. Syuhairi |, M. Husain (2013) Numerical simulation of a low aspect ratio wing at low Reynolds number. In: 2nd International Conference on Mechanical, Automotive and Aerospace Engineering (ICMAAE' 13), 2-4 July 2013, Kuala Lumpur, Malaysia. (Unpublished) |
| spellingShingle | TL500 Aeronautics Suliman , M. M. Ali Omar, Ashraf Ali Syed Mohamed Ali, Jaffar M. Syuhairi |, M. Husain Numerical simulation of a low aspect ratio wing at low Reynolds number |
| title | Numerical simulation of a low aspect ratio wing at low Reynolds number |
| title_full | Numerical simulation of a low aspect ratio wing at low Reynolds number |
| title_fullStr | Numerical simulation of a low aspect ratio wing at low Reynolds number |
| title_full_unstemmed | Numerical simulation of a low aspect ratio wing at low Reynolds number |
| title_short | Numerical simulation of a low aspect ratio wing at low Reynolds number |
| title_sort | numerical simulation of a low aspect ratio wing at low reynolds number |
| topic | TL500 Aeronautics |
| url | http://irep.iium.edu.my/33139/ http://irep.iium.edu.my/33139/1/Paper_30161_-_Camera_ready.pdf http://irep.iium.edu.my/33139/4/programbookicmaae13.pdf |