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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Bibliographic Details
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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Summary: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)