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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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Bug in Calculating xi from x #6

Open ddmarshall opened 1 year ago

ddmarshall commented 1 year ago

All(?) cambered airfoils using the orthogonal construction will have a small region near leading edge where x<0, but current implementation cannot recover the xi for these points because there is an assumption of 0<=x<=1.