Thin Aerofoil Theory
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This form calculates the lift and pitching moment properties of a two dimensional
aerofoil section using the mean line, thin aerofoil theory. The section data can be
loaded from file (see nacacalc.php for required format). In order to analyse a section you need to first select an Aerofoil Section Data File that you have saved on your computer. Use "Browse..." to find and select a file. Then Click "Upload" to send the file to the server to start the analysis process. | ||
Input Parameters
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