Xfoil Interface 1.0

This simple function will use a system call to run Xfoil. It then loads the results into a data structure which you can then use in your Matlab script.For example to deflect the trailing edge of a NACA0009 by 5deg at 65% chord and run multiple incidence angles...[pol foil] = xfoil('NACA0009',[-5:15],1e6,0.2,'oper iter 150','gdes flap 0.65 0 5 exec')The coefficents will be returned in the pol structure while the foil data and pressure distribution will be returned in foil structure.XFOIL, first developed by Mark Drela at MIT, is a program for the design and analysis of subsonic isolated airfoils and is released under the GNU General Public License.

Requirements:	No special requirements
Platforms:	Matlab
Keyword:	Airfoils,  Analysis,  And Is,  Anglespol Foil,  At 65,  Chord,  Deflect,  Deg,  Foil,  Gdes Flap,  Gnu,  Matlab Scriptfor,  Mit,  Pressure,  Run,  Run Xfoil,  Simple Function,  Which You Can,  Xfoil Naca Oper
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