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2-D CFD Analysis of Ring Air foil UAV


Author(s):

A. Aravindkumar , Government college of technology; Dr. S. Periyasamy, Government college of technology

Keywords:

UAV, Ring Airfoil, L/D Ratio, Fan, Stall Angle

Abstract:

In this paper examined the aerodynamic behaviour of ring airfoil UAV. The ring airfoil is non-planar wing like disk shape and its cross-section like mirrored airfoil with respect to the vertical axis. Ring airfoil increase UAV VTOL performance. In numerical analysis of ring airfoil cross-section to find lift, drag and L/D ratio with respect to the different angle of attack and various velocities. k-ε turbulent model is use numerical analysis in fluent.


Other Details:

Manuscript Id :IJSTEV3I7108
Published in :Volume : 3, Issue : 7
Publication Date: 01/02/2017
Page(s): 192-195
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