• MOHAMMED DANISH
• NEETESH KUMAR
• S SATISH REDDY
• RAMESH KUMAR S C

In this work, NACA M2 aerofoil was analyzed. The analysis carried out was by varying wind velocities and angles of attack of NACA M2 aerofoil model. Analysis is performed experimentally in the wind tunnel testing facility and similarly CFD analysis is performed to obtain various parameters such as Cl (coefficient of lift), Cd (coefficient of drag) & Cp (coefficient of pressure).We have fabricated NACA M2 aerofoil model using composite material and its size considering the experimental setup dimensions. The natures of the graphs of comparative analysis were found to be similar. Similarly, for NACA 0008 aerofoil we have performed CFD analysis and obtained velocity and pressure contour. On the basis of CFD and experimental results we can conclude that NACA M2 aerofoil has better coefficient of lift and coefficient of drag, on this basis we can say that NACA M2 aerofoil comparatively can be a substitute for various e-MAV application.

Coefficient of drag, Coefficient of lift, Computational Fluid Dynamics, NACA M2 , NACA 0008

"Numerical and Experimental Analysis of Aerofoil for electric -Manned Air Vehicle (e-MAV)", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 5, page no.289-296, May-2019, Available :http://www.jetir.org/papers/JETIRBZ06046.pdf

"Numerical and Experimental Analysis of Aerofoil for electric -Manned Air Vehicle (e-MAV)", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 5, page no. pp289-296, May-2019, Available at : http://www.jetir.org/papers/JETIRBZ06046.pdf