Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft
In this paper, three dimensional data and behavior of incompressible and steady air flow around a small scale Wing in Ground Effect Craft (WIG) were investigated and studied numerically then compared to the experimental result and also published data. This computational simulation (CFD) adopted two...
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my.utm.591952021-12-13T02:46:17Z http://eprints.utm.my/id/eprint/59195/ Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft Baharun, A. Tarmizi Maimun, Adi Ahmed, Yasser M. Mobassher, M. Nakisa, M. TJ Mechanical engineering and machinery In this paper, three dimensional data and behavior of incompressible and steady air flow around a small scale Wing in Ground Effect Craft (WIG) were investigated and studied numerically then compared to the experimental result and also published data. This computational simulation (CFD) adopted two turbulence models, which were k-ε and k-ω in order to determine which model produces minimum difference to the experimental result of the small scale WIG tested in wind tunnel. Unstructured mesh was used in the simulation and data of drag coefficient (Cd) and lift coefficient (Cl) were obtained with angle of attack (AoA) of the WIG model as the parameter. Ansys ICEM was used for the meshing process while Ansys Fluent was used for solution. Aerodynamic forces, Cl, Cd and Cl/Cd along with fluid flow pattern of the small scale WIG craft was shown and discussed. 2015 Conference or Workshop Item PeerReviewed Baharun, A. Tarmizi and Maimun, Adi and Ahmed, Yasser M. and Mobassher, M. and Nakisa, M. (2015) Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft. In: International Conference on Mathematics, Engineering and Industrial Applications, ICoMEIA 2014, 28 - 30 May 2014, Penang, Malaysia. http://dx.doi.org/10.1063/1.4915838 |
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TJ Mechanical engineering and machinery Baharun, A. Tarmizi Maimun, Adi Ahmed, Yasser M. Mobassher, M. Nakisa, M. Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft |
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In this paper, three dimensional data and behavior of incompressible and steady air flow around a small scale Wing in Ground Effect Craft (WIG) were investigated and studied numerically then compared to the experimental result and also published data. This computational simulation (CFD) adopted two turbulence models, which were k-ε and k-ω in order to determine which model produces minimum difference to the experimental result of the small scale WIG tested in wind tunnel. Unstructured mesh was used in the simulation and data of drag coefficient (Cd) and lift coefficient (Cl) were obtained with angle of attack (AoA) of the WIG model as the parameter. Ansys ICEM was used for the meshing process while Ansys Fluent was used for solution. Aerodynamic forces, Cl, Cd and Cl/Cd along with fluid flow pattern of the small scale WIG craft was shown and discussed. |
format |
Conference or Workshop Item |
author |
Baharun, A. Tarmizi Maimun, Adi Ahmed, Yasser M. Mobassher, M. Nakisa, M. |
author_facet |
Baharun, A. Tarmizi Maimun, Adi Ahmed, Yasser M. Mobassher, M. Nakisa, M. |
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Baharun, A. Tarmizi |
title |
Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft |
title_short |
Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft |
title_full |
Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft |
title_fullStr |
Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft |
title_full_unstemmed |
Comparison of numerical simulation with experimental result for small scale one seater Wing in Ground Effect (WIG) craft |
title_sort |
comparison of numerical simulation with experimental result for small scale one seater wing in ground effect (wig) craft |
publishDate |
2015 |
url |
http://eprints.utm.my/id/eprint/59195/ http://dx.doi.org/10.1063/1.4915838 |
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1720436901271306240 |
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13.211869 |