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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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Hess-Smith Method Not Complete #7

Open ddmarshall opened 1 year ago

ddmarshall commented 1 year ago

Hess-Smith method cannot model lifting airfoils. Need to add vortex component to calculation after have airfoil geometry ready to be used.