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Design and Flow Analysis over Airfoil with Hexagonal Dimples and its Effects by ANSYS (Fluent) Software

Author(s):
Mr. V. Nivash , Sri Shanmugha College of Engineering and Technology; Mr. S. Manikandan, Sri Shanmugha College of Engineering and Technology; Mr. S M. Meyvel, Sri Shanmugha College of Engineering and Technology; Mr. K J. Nethaji, Sri Shanmugha College of Engineering and Technology; Mr. N. Kavin, Sri Shanmugha College of Engineering and Technology

Keywords:
Airfoil, Hexagonal Dimples, Separation Point, Lift Force, Drag Force, Angle of Attack

Abstract

This paper describe how to reduce the drag force and increase the lift force in aircraft airfoils by increasing separation point in making of hexagonal shape of dimples in both inward and outward side separate airfoil models by using ANSYS (Fluent) software design.

Other Details
Paper ID: IJSRDV6I10493
Published in: Volume : 6, Issue : 1
Publication Date: 01/04/2018
Page(s): 1295-1300

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