I’m trying to match drag and lift coefficient vs. alpha using a NACA0010 with the results online on airfoiltools.com. My trend looks like it is matching very well, but the values are somewhat off. What values/factors in the simulation designer should I change in order to get the values to be somewhat closer?
Here’s a link to my simulation on simscale: https://www.simscale.com/projects/ejohnathon/naca0010/
Actual coefficient is the data from airfoiltools.com
Experimental coefficient is the data I got using simscale