**Last Updated: 4/29/2014**

**Panel
Method Spreadsheet (Updated 4/29/2014)**

This workbook
implements the vortex panel method for a 2D airfoil. The algorithm is from Kuethe and
Chow, *Foundations of Aerodynamics*, 4^{th}
Edition, Wiley (1986). Inputs
are coordinate data for the airfoil (from a source such as Abbott and von
Doenhoff, *Theory of Wing Sections*, _{p} as a function of position and a
streamline plot.

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