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Design and Performance Analysis of Airfoil By Low Reynolds Number Method Using CFD

Author(s):

Dilip Muchhala , Institute of Engineering and Technology, davv Indore; santosh kansal, Institute of Engineering and Technology, davv Indore

Keywords:

NACA0018, CFD FLUENT, Attack angle, Pressure difference, Shape Design, Analysis of Airfoil

Abstract

The present work deal with the design and performance analysis of NACA0018 airfoil with the use of viscous laminar model of FLUENT and also comparative analysis with standard experimental results. It also comprises the various angle of attack (00,40, 80) with respective variation in coefficient of lift (CL) and coefficient of drag (CD). In this numerical study we use low Reynolds number Airfoil design method.

Other Details

Paper ID: IJSRDV4I30921
Published in: Volume : 4, Issue : 3
Publication Date: 01/06/2016
Page(s): 1114-1116

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