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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