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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Main Author: Gopal Krishnan, Sivaraj
Format: Thesis
Language:English
Published: 2017
Subjects:
Online Access:http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf
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spelling my-usm-ep.464222021-11-17T03:42:17Z Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet 2017-01-01 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 Thesis http://eprints.usm.my/46422/ http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuruteraan Aeroangkasa
institution Universiti Sains Malaysia
collection USM Institutional Repository
language English
topic T Technology
T Technology
spellingShingle T Technology
T Technology
Gopal Krishnan, Sivaraj
Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet
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)
format Thesis
qualification_level Master's degree
author Gopal Krishnan, Sivaraj
author_facet Gopal Krishnan, Sivaraj
author_sort Gopal Krishnan, Sivaraj
title 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_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_sort investigation of aerodynamic characteristics of a wing model with rgv winglet
granting_institution Universiti Sains Malaysia
granting_department Pusat Pengajian Kejuruteraan Aeroangkasa
publishDate 2017
url http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf
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