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Analysis of NACA 4412 and NACA 0018 Airfoil: A Review

Author(s):
Yash Dhaduk , PARUL INSTITUTE OF ENGINEERING & TECHNOLOGY; Ankitkumar Patel, PARUL INSTITUTE OF ENGINEERING & TECHNOLOGY-DS; Karnailsingh Saini, PARUL INSTITUTE OF ENGINEERING & TECHNOLOGY-DS

Keywords:
Flow Over an Airfoil, AOA, Aerodynamics, Lift and Drag Force, Coefficient of Lift, Coefficient of Drag, Ansys Fluent

Abstract

This report is aimed to obtain the velocity and pressure profile, production of Lift and Drag by Airfoil at particular AOA, separation of flow over an Airfoil, the graph of variation in coefficient of lift with AOA (cl-α) and coefficient of Drag with AOA (cd-α) is plotted by using the Ansys Software for an NACA 4412 and NACA 0018 Airfoil. We use fluent module in Ansys for Analysis. CFD plays an important role in design and optimization process. In this project we are comparing the Computational result with the standard result.

Other Details
Paper ID: IJSRDV7I10602
Published in: Volume : 7, Issue : 1
Publication Date: 01/04/2019
Page(s): 916-920

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