reorganize file structure

airfoil/airfoil.m

@@ -0,0 +1,24 @@
+%ASCorrea
+
+function airfoil(airfoilfilename)
+
+rootLOCATION='\\ad.uiuc.edu\ae\correa2\Desktop\AE441\AE441 - Home Edition\Matlab code\';
+airfoilLOCATION='\\ad.uiuc.edu\ae\correa2\Desktop\AE441\AE441 - Home Edition\Airfoils';
+
+
+% airfoilfilename=input('Input airfoil dat file: \nNote: You must delete the header before using \n:','s');
+% airfoilfilename='flatplate.dat'
+cd(airfoilLOCATION)
+data=load(airfoilfilename);
+plottitle=regexprep(airfoilfilename, '.dat', '');
+
+dataX=data(:,1);
+dataY=data(:,2);
+
+plot(dataX, dataY, 'k', 'LineWidth', 2)
+axis equal
+axis off
+title(['Airfoil ' , plottitle])
+print ('-dtiff', plottitle)
+cd(rootLOCATION)
+end