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.
Volume/Issue: Volume. 6 - Issue. 09 , September - 2017
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 Reynoldsâ€™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.
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