Paper Details

Title	Computational Study of NACA0012 Using Micro Cylinder at Low Reynolds Number
Author	Mohd. Umar, Faisal Shameem
Abstract	To achieve aerodynamic efficiency, the effect of passive flow plays a vital role and has been the area of interest for research. Due to small modifications in geometry the improvement in performance can be observed. The Computational study on NACA0012 was performed at low reynolds number by placing micro cylinder near its leading edge and investigating the results of lift and drag coefficients at different angle of attack.
Keywords	Micro Aerial Vehicle, Airfoil, Viscosity, Micro-cylinder, Reynolds Number
Page Number	8-16
Date of Publication	2024-06-30
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