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ddmarshall / panel-code

Libraries and Resources for panel codes used to model aerodynamic flows.
GNU General Public License v3.0
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Airfoil Leading Edge Properties #5

Open ddmarshall opened 1 year ago

ddmarshall commented 1 year ago

Some properties at the leading edge are undefined (x_p, y_p, etc.) but some have finite values (dy/dx, k, etc.). Need to short-circuit regular calculations when close to the leading edge (<1e-7) to get these finite values.

ddmarshall commented 1 year ago

This should be done after the geometry->airfoil->etc. hierarchy is set. This will requiring overriding common methods but only in certain situations.