petebachant/actuatorLine-2D-turbinesFoam
2-D static airfoil simulated with the turbinesFoam actuator line model.
NACA 0020 OpenFOAM case for studying blade end effects.
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2-D static airfoil simulated with the turbinesFoam actuator line model.
Array optimization using the turbinesFoam actuator line model.
Slides for my Fall 2015 UNH ME grad seminar talk.
NACA XX20 airfoil coefficients calculated with XFOIL via QBlade.