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...

全面介紹

Saved in:
書目詳細資料
主要作者: Gopal Krishnan, Sivaraj
格式: Thesis
語言:English
出版: 2017
主題:
在線閱讀:http://eprints.usm.my/46422/1/Investigation%20Of%20Aerodynamic%20Characteristics%20Of%20A%20Wing%20Model%20With%20Rgv%20Winglet.pdf
標簽: 添加標簽
沒有標簽, 成為第一個標記此記錄!
實物特徵
總結: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)