Paper Key : IRJ************887
Author: Hithesh Nabiraj
Date Published: 11 Nov 2024
Abstract
This paper presents the analysis of the various aerodynamic properties like lift and drag, with respect to the followingairfoils: NACA 22112, NACA 23015, NACA 23018, NACA 23021, NACA 23112, NACA 24112. The objective ofthis study is to explore the effects of lift and drag at various angles to find out how efficiently it can perform under awide range of conditions. The Cd, Cl and Alpha for the NACA 5-digit series airfoils are taken from the airfoil toolswebsite. The data is then calculated to evaluate the Cl vs Alpha, Cd vs Alpha, Cl vs Cd and ClCd vs Alpha values,that is then plotted onto their respective graphs for further investigation. This shows us that there are some airfoils thathave properties that allow them to perform better under conditions where other airfoils might stagger.
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