First of all, I'm glad everyone is so interested in my work. I'm really sorry that I haven't been able to check in here more often to help people out. Quite frankly the code I wrote does its job well enough for me, and I had no idea it would get as popular as it did. I'm thinking of getting a SourceForge page and making this a full-blown project. If there's anyone out there willing to help me out here, let me know - please PM me and we can discuss privately.
I think I've got enough time now to start working on this more generally. Here's the function call for the framework I'm thinking of:
Originally Posted by aaepl
So you are required to specify airfoil, Re, Ma, and alfa_start; maxit will default to some number, alfa_end and alfa_step are only used when you want to do a MATLAB aseq command, since that's much more efficient than calling this function over and over again in a for loop.
function [CL,CD,CM, Xcp] = xfoil(airfoil, Re, Ma, maxit, alfa_start, alfa_end, alfa_step)
Other ideas for what needs to go in?
Also could you post or send me your modifications? I'd like to incorporate them if they're already working. (Of course when this is released you will get full credit - I'd like to release under the GPL or something.)