IJERT-EMS
IJERT-EMS

Study and Analyse Airfoil Section using CFD


Study and Analyse Airfoil Section using CFD
Authors : Rajat Veer, Kiran Shinde, Vipul Gaikwad , Pritam Sonawane, Yogesh Sonawane
Publication Date: 08-09-2017

Authors

Author(s):  Rajat Veer, Kiran Shinde, Vipul Gaikwad , Pritam Sonawane, Yogesh Sonawane

Published in:   International Journal of Engineering Research & Technology

License:  This work is licensed under a Creative Commons Attribution 4.0 International License.

Website: www.ijert.org

Volume/Issue:   Volume. 6 - Issue. 09 , September - 2017

e-ISSN:   2278-0181

 DOI:  http://dx.doi.org/10.17577/IJERTV6IS090028

Abstract

In this report coefficient of drag and coefficient of lift is obtained with the help of CFD, it is also obtained by an experiment which is conducted on wind tunnel. Though both of the methods give approximate result for the same test section, an experimental process has greater cost and quite laborious than that of CFD. Analysis of airfoil over two-dimensional subsonic flow at a various angle of attacks and operating at Reynolds’s number is obtained. The result shown by CFD has closely agreed with experiment result, thus CFD is a mature tool to predict the performance of test section at any angle of attack.

Citations

Number of Citations for this article:  Data not Available

Keywords

Key Word(s):    

Downloads

Number of Downloads:     21
Similar-Paper

Call for Papers - May - 2017

        

 

                 Call for Thesis - 2017 

     Publish your Ph.D/Master's Thesis Online

              Publish Ph.D Master Thesis Online as Book