Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet
This work describes the aerodynamic characteristics of an aircraft model wing with RGV winglet. A Computational Fluid Dynamics (CFD) study using ANSYS 15.0 is conducted to study the effect of the RGV winglet on a rectangular wing. The wing consists of 660 mm span and 121 mm chord length where the...
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Format: | Thesis |
Language: | English |
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2017
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Online Access: | http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf |
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author | Gopal Krishnan, Sivaraj |
author_facet | Gopal Krishnan, Sivaraj |
author_sort | Gopal Krishnan, Sivaraj |
collection | USM |
description | This work describes the aerodynamic characteristics of an aircraft model wing with
RGV winglet. A Computational Fluid Dynamics (CFD) study using ANSYS 15.0 is
conducted to study the effect of the RGV winglet on a rectangular wing. The wing
consists of 660 mm span and 121 mm chord length where the aspect ratio is 5.45. The
NACA 65(3) |
first_indexed | 2024-03-06T15:36:15Z |
format | Thesis |
id | usm.eprints-46422 |
institution | Universiti Sains Malaysia |
language | English |
last_indexed | 2024-03-06T15:36:15Z |
publishDate | 2017 |
record_format | dspace |
spelling | usm.eprints-464222021-11-17T03:42:17Z http://eprints.usm.my/46422/ Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet Gopal Krishnan, Sivaraj T Technology TL500-777 Aeronautics. Aeronautical engineering This work describes the aerodynamic characteristics of an aircraft model wing with RGV winglet. A Computational Fluid Dynamics (CFD) study using ANSYS 15.0 is conducted to study the effect of the RGV winglet on a rectangular wing. The wing consists of 660 mm span and 121 mm chord length where the aspect ratio is 5.45. The NACA 65(3) 2017-01-01 Thesis NonPeerReviewed application/pdf en http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf Gopal Krishnan, Sivaraj (2017) Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet. Masters thesis, Universiti Sains Malaysia. |
spellingShingle | T Technology TL500-777 Aeronautics. Aeronautical engineering Gopal Krishnan, Sivaraj Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet |
title | Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet |
title_full | Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet |
title_fullStr | Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet |
title_full_unstemmed | Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet |
title_short | Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet |
title_sort | investigation of aerodynamic characteristics of a wing model with rgv winglet |
topic | T Technology TL500-777 Aeronautics. Aeronautical engineering |
url | http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf |
work_keys_str_mv | AT gopalkrishnansivaraj investigationofaerodynamiccharacteristicsofawingmodelwithrgvwinglet |