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...
| Main Author: | |
|---|---|
| Format: | Thesis |
| Language: | English |
| Published: |
2017
|
| Subjects: | |
| Online Access: | http://eprints.usm.my/46422/ http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf |
| _version_ | 1848880604328755200 |
|---|---|
| author | Gopal Krishnan, Sivaraj |
| author_facet | Gopal Krishnan, Sivaraj |
| author_sort | Gopal Krishnan, Sivaraj |
| building | USM Institutional Repository |
| collection | Online Access |
| 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 | 2025-11-15T18:05:46Z |
| format | Thesis |
| id | usm-46422 |
| institution | Universiti Sains Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T18:05:46Z |
| publishDate | 2017 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | usm-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/ http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf |