How to Calculate Reynolds Number for Airfoil?
Reynolds Number for Airfoil calculator uses Reynolds Number = (Density of Fluid*Flow Velocity*Chord Length of Airfoil)/Dynamic Viscosity to calculate the Reynolds Number, The Reynolds Number for airfoil is a dimensionless value that is used to determine whether the fluid is exhibiting laminar flow (R less than 2300) or turbulent flow (R greater than 4000). Reynolds Number is denoted by Re symbol.
How to calculate Reynolds Number for Airfoil using this online calculator? To use this online calculator for Reynolds Number for Airfoil, enter Density of Fluid (ρfluid), Flow Velocity (Vf), Chord Length of Airfoil (c) & Dynamic Viscosity (μviscosity) and hit the calculate button. Here is how the Reynolds Number for Airfoil calculation can be explained with given input values -> 0.605294 = (1.225*1.12*0.45)/1.02.